MTS SWIFT 30 User Manual

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SWIFT® 30 Sensor Product Information
Spinning Wheel Integrated Force Transducer
For Passenger Vehicles
100-026-689 F
Copyright information © 1999, 2000, 2005, 2006, 2008 MTS Systems Corporation. All rights reserved.
Trademark information MTS, SWIFT, TestStar, and TestWare are registered trademarks of MTS Systems
Corporation within the United States. These trademarks may be protected in other countries.
Microsoft, Windows, Windows for Workgroups, Windows 95, and Windows NT are registered trademarks of Microsoft Corporation. Apple and Macintosh are registered trademarks of Apple Computer, Inc. UNIX is a registered trademark of The Open Group. All other trademarks or service marks are property of their respective owners.
Publication information
MANUAL PART NUMBER PUBLICATION DATE
151956-00 B February 1999
100-026-689 A June 2000
100-026-689 B July 2000
100-026-689 C May 2005
100-026-689 D October 2005
100-026-689 E January 2006
100-026-689 F November 2008
Contents
Technical Support 7
How to Get Technical Support 7
Before You Contact MTS 7
If You Contact MTS by Phone 9
Problem Submittal Form in MTS Manuals 10
Preface 11
Before You Begin 11
Conventions 12
Documentation Conventions 12
Hardware Overview 15
Spinning Applications (Test Track) 16
Non-spinning Applications (Simulation Lab) 17
Construction 18
Design Features 22
Coordinate System 23
Specifications 25
Calibration 29
Transducer Interface 31
TI Front Panel 34
TI Rear Panel 41
TI Jumpers 42
Interfacing with RPC 43
Software Utilities 45
Introduction 46
TISTATUS - Transducer Interface Status 47
TIXFER - Transducer Interface Transfer 48
TISHUNT - Transducer Interface Shunt 50
Setting Up Shunt Calibration Reference Values 54
TISETZERO – Transducer Interface Set Zero Method 55
Error Messages 56
SWIFT 30 Sensors Contents
Shunt Error Status 57
Setting up the Transducer Interface 59
Select a Zero Method 60
Calibration File Elements 61
Zero Algorithms 62
Upload the Calibration File 64
Edit the Calibration File 66
Download the Calibration File 70
Installing the Transducer 73
Test Track Vehicle 74
Attaching SWIFT Components to the Vehicle 78
Attaching SWIFT and Wheel Assembly to the Vehicle 81
Installing the Transducer Interface Electronics 83
Setting up the SWIFT Sensor for Data Collection 85
Verifying the Quality of the Zero Procedure 95
Collecting Data 97
Road Simulator 99
Attaching SWIFT Components to the Fixturing 101
Zeroing the Transducer Interface 104
Communication Configurations 105
Cable Configurations 106
SWIFT TI to PC Host (9-pin) 106
SWIFT TI to PC Host (25-pin) 106
SWIFT TI to SWIFT TI 106
Termination Jumper 107
Analyzing SWIFT Data 109
The Data 110
Fx Data (Longitudinal Force) 111
Fz Data (Vertical Force) 113
Mx Data (Overturning Moment) 114
My Data (Brake Moment) 117
Acceleration and Braking Events Example 119
Slalom Curve Driving Example 121
Contents
SWIFT 30 Sensors
Maintenance 123
Transducer 124
Transducer Interface 125
Cables 126
Troubleshooting 127
Assembly Drawings 141
Cable Drawings 142
SWIFT 30 Mechanical Parts 157
Common Parts 165
SWIFT 30 Sensors Contents
Contents
SWIFT 30 Sensors

Technical Support

How to Get Technical Support

Start with your
manuals
Technical support
methods
MTS web site
www.mts.com
E-mail techsupport@mts.com
Telephone MTS Call Center 800-328-2255
Fax 952-937-4515
Technical support
outside the U.S.
The manuals supplied by MTS provide most of the information you need to use and maintain your equipment. If your equipment includes MTS software, look for online help and README files that contain additional product information.
If you cannot find answers to your technical questions from these sources, you can use the internet, e-mail, telephone, or fax to contact MTS for assistance.
MTS provides a full range of support services after your system is installed. If you have any questions about a system or product, contact MTS in one of the following ways.
The MTS web site gives you access to our technical support staff by means of a Technical Support link:
www.mts.com > Contact MTS > Service & Technical Support
Weekdays 7:00 A.M. to 5:00 P.M., Central Time
Please include “Technical Support” in the subject line.
For technical support outside the United States, contact your local sales and service office. For a list of worldwide sales and service locations and contact information, use the Global MTS link at the MTS web site:
www.mts.com > Global MTS > (choose your region in the right-hand column) > (choose the location closest to you)

Before You Contact MTS

MTS can help you more efficiently if you have the following information available when you contact us for support.
Know your site
number and system
number
SWIFT 30 Sensors Technical Support
The site number contains your company number and identifies your equipment type (material testing, simulation, and so forth). The number is usually written on a label on your MTS equipment before the system leaves MTS. If you do not have or do not know your MTS site number, contact your MTS sales engineer.
Example site number: 571167
When you have more than one MTS system, the system job number identifies which system you are calling about. You can find your job number in the papers sent to you when you ordered your system.
Example system number: US1.42460
Know information from
prior technical
If you have contacted MTS about this problem before, we can recall your file. You will need to tell us the:
assistance
MTS notification number
Name of the person who helped you
Identify the problem Describe the problem you are experiencing and know the answers to the
following questions:
How long and how often has the problem been occurring?
Can you reproduce the problem?
Were any hardware or software changes made to the system before the
problem started?
What are the model numbers of the suspect equipment?
What model controller are you using (if applicable)?
What test configuration are you using?
Know relevant
computer information
Know relevant
software information
If you are experiencing a computer problem, have the following information available:
Manufacturer’s name and model number
Operating software type and service patch information
Amount of system memory
Amount of free space on the hard drive in which the application resides
Current status of hard-drive fragmentation
Connection status to a corporate network
For software application problems, have the following information available:
The software application’s name, version number, build number, and if
available, software patch number. This information is displayed briefly when you launch the application, and can typically be found in the “About” selection in the “Help” menu.
It is also helpful if the names of other non-MTS applications that are
running on your computer, such as anti-virus software, screen savers, keyboard enhancers, print spoolers, and so forth are known and available.
Technical Support
SWIFT 30 Sensors

If You Contact MTS by Phone

Your call will be registered by a Call Center agent if you are calling within the United States or Canada. Before connecting you with a technical support specialist, the agent will ask you for your site number, name, company, company address, and the phone number where you can normally be reached.
If you are calling about an issue that has already been assigned a notification number, please provide that number. You will be assigned a unique notification number about any new issue.
Identify system type To assist the Call Center agent with connecting you to the most qualified
technical support specialist available, identify your system as one of the following types:
Electromechanical materials test system
Hydromechanical materials test system
Vehicle test system
Vehicle component test system
Aero test system
Be prepared to
troubleshoot
Write down relevant
information
After you call MTS logs and tracks all calls to ensure that you receive assistance and that action
Prepare yourself for troubleshooting while on the phone:
Call from a telephone when you are close to the system so that you can try
implementing suggestions made over the phone.
Have the original operating and application software media available.
If you are not familiar with all aspects of the equipment operation, have an
experienced user nearby to assist you.
Prepare yourself in case we need to call you back:
Remember to ask for the notification number.
Record the name of the person who helped you.
Write down any specific instructions to be followed, such as data recording
or performance monitoring.
is taken regarding your problem or request. If you have questions about the status of your problem or have additional information to report, please contact MTS again and provide your original notification number.
SWIFT 30 Sensors Technical Support

Problem Submittal Form in MTS Manuals

Use the Problem Submittal Form to communicate problems you are experiencing with your MTS software, hardware, manuals, or service which have not been resolved to your satisfaction through the technical support process. This form includes check boxes that allow you to indicate the urgency of your problem and your expectation of an acceptable response time. We guarantee a timely response—your feedback is important to us.
The Problem Submittal Form can be accessed:
In the back of many MTS manuals (postage paid form to be mailed to MTS)
www.mts.com > Contact Us > Problem Submittal Form (electronic form to
be e-mailed to MTS)
Technical Support
10
SWIFT 30 Sensors

Preface

Before You Begin

Safety first! Before you attempt to use your MTS product or system, read and understand the
Safety manual and any other safety information provided with your system. Improper installation, operation, or maintenance of MTS equipment in your test facility can result in hazardous conditions that can cause severe personal injury or death and damage to your equipment and specimen. Again, read and understand the safety information provided with your system before you continue. It is very important that you remain aware of hazards that apply to your system.
Other MTS manuals In addition to this manual, you may receive additional MTS manuals in paper or
electronic form.
If you have purchased a test system, it may include an MTS System Documentation CD. This CD contains an electronic copy of the MTS manuals that pertain to your test system, including hydraulic and mechanical component manuals, assembly drawings and parts lists, and operation and preventive maintenance manuals. Controller and application software manuals are typically included on the software CD distribution disc(s).
SWIFT 30 Sensors Preface
11

Conventions

DANGER
WARNING
CAUTION
Conventions

Documentation Conventions

The following paragraphs describe some of the conventions that are used in your MTS manuals.
Hazard conventions As necessary, hazard notices may be embedded in this manual. These notices
contain safety information that is specific to the task to be performed. Hazard notices immediately precede the step or procedure that may lead to an associated hazard. Read all hazard notices carefully and follow the directions that are given. Three different levels of hazard notices may appear in your manuals. Following are examples of all three levels.
Note For general safety information, see the safety information provided with
your system.
Danger notices indicate the presence of a hazard with a high level of risk which, if ignored, will result in death, severe personal injury, or substantial property damage.
Warning notices indicate the presence of a hazard with a medium level of risk which, if ignored, can result in death, severe personal injury, or substantial property damage.
Caution notices indicate the presence of a hazard with a low level of risk which, if ignored, could cause moderate or minor personal injury, equipment damage, or endanger test integrity.
Notes Notes provide additional information about operating your system or highlight
easily overlooked items. For example:
Note Resources that are put back on the hardware lists show up at the end of
the list.
Special terms The first occurrence of special terms is shown in italics.
Illustrations Illustrations appear in this manual to clarify text. It is important for you to be
aware that these illustrations are examples only and do not necessarily represent your actual system configuration, test application, or software.
Electronic manual
conventions
This manual is available as an electronic document in the Portable Document File (PDF) format. It can be viewed on any computer that has Adobe Acrobat Reader installed.
12
Preface
SWIFT 30 Sensors
Conventions
Hypertext links The electronic document has many hypertext links displayed in a blue font. All
blue words in the body text, along with all contents entries and index page numbers, are hypertext links. When you click a hypertext link, the application jumps to the corresponding topic.
SWIFT 30 Sensors Preface
13
Conventions
14
Preface
SWIFT 30 Sensors

Hardware Overview

Data
S20-25
Test Track
Laboratory Simulation
Overview The MTS Spinning Wheel Integrated Force Transducer (SWIFT
weight, easy-to-use transducer that enables you to conduct faster, less expensive data acquisition and road simulation testing.
The transducer is designed for use both on the test track and in the test laboratory. It attaches to the test vehicle or an MTS Series 329 Road Simulator using an adapter and a modified wheel rim.
You can achieve excellent data correlation using the same transducer and vehicle on the test track and on a road simulator. It is available in various sizes and materials to fit various vehicle and loading requirements.
®
) is a light-
Contents Spinning Applications (Test Track) 16
Non-spinning Applications (Simulation Lab) 17
Construction 18
Design Features 22
Coordinate System 23
Specifications 25
Calibration 29
Transducer Interface 31
TI Front Panel 34
TI Rear Panel 41
TI Jumpers 42
Interfacing with RPC 43
SWIFT 30 Sensors Hardware Overview
15

Spinning Applications (Test Track)

Customer Supplied
12 Vdc Power Supply
Customer Supplied
Data Recorder
Transducer Interface
(TI)
Transducer Signals
Output
Signals
S20-26
Spinning Applications (Test Track)
The SWIFT sensor can be used for road load data acquisition (RLDA) applications:
Durability
Noise, Vibration and Harshness (NVH)
Ride and Handling
Tire Performance
The transducer is durable enough to withstand harsh road testing and data acquisition environments. The transducer is splash resistant and suitable for use in conditions where the test vehicle will encounter occasional standing or running water, or will be exposed to precipitation. However, it should not be submerged.
In a typical spinning application, the transducer is mounted on a modified rim of a tire on a test vehicle, as shown in the following figure. The Transducer Interface (TI), power supply, and data recorder can be located inside the vehicle or in the trunk..
Hardware Overview
16
Spinning Application (Test Track)
SWIFT 30 Sensors

Non-spinning Applications (Simulation Lab)

12 Vdc Power Supply
(with 4 connections)
Customer Supplied
Data Recorder
Transducer Interface
(TI)
Transducer Signals
Output
Signals
PC
Communication
S20-27
Non-spinning Applications (Simulation Lab)
The SWIFT sensor can be fully integrated into the simulation process, since it is an optimal feedback transducer for use with MTS Remote Parameter Control
®
) software. The transducer takes data at points where fixturing inputs are
(RPC located rather than at traditional instrumentation points along the vehicle’s suspension. Using the SWIFT sensor saves you instrumentation time, and fewer iterations are required to achieve good simulation accuracy.
Measuring spindle loads allows engineers to generate generic road profiles. Generic road profiles are portable across various vehicle models, do not require new test track load measurements for each vehicle, and eliminate additional RLDA tasks.
Four of the six loads measured by the transducer directly correlate to the MTS Model 329 Road Simulator inputs: vertical force, longitudinal force, lateral force, and braking input.
The same transducers used to collect road data at the test track can be mounted directly in the wheel adapters of the MTS Model 329 Road Simulator. For durability testing, an aluminum SWIFT sensor can be used for iterations within the RPC process. The aluminum SWIFT sensor should then be removed for the durability cycles, to preserve its fatigue life. It can be replaced by an adapter plate, available from MTS, to duplicate the mass and center of gravity of the actual SWIFT sensor. If a SWIFT sensor is to be used during full durability tests, we suggest using the titanium model, which has a higher fatigue rating.
®
In a typical non-spinning application, a SWIFT sensor is mounted on a road simulation test fixture, as shown in the following figure.
Non-spinning Application (Laboratory Simulation)
SWIFT 30 Sensors Hardware Overview
17

Construction

S20-03
Transducer
Hub Adapter
Slip Ring
(with Encoder)
Modified
Wheel Rim
Slip Ring
Bracket (Spider)
Construction
The SWIFT sensor has one-piece construction for outstanding fatigue life, low hysteresis, and high stiffness. Its compact package has a minimal effect on inertia calculations, and a minimal dynamic effect on the test vehicle.
The transducer can be used for developing conventional durability tests on the MTS Model 329 Road Simulator. Normally, the transducer is replaced with an equivalent wheel adapter after the simulation drive signals are developed and prior to the start of the test.
The SWIFT sensor includes several mechanical and electrical components.
Transducer The transducer attaches directly to a modified wheel rim. On the test track, it
spins with the wheel. It does not spin on a road simulator. The transducer is available in two materials: aluminum for spinning applications where the priority is on light weight, and titanium for non-spinning applications, where the priority is on durability.
The transducer’s unibody design means there are no multiple parts welded or screwed together.
The transducer has four beams with strain gages that measure six orthogonal outputs:
Fx—longitudinal force
Fy—lateral force
Fz—vertical force
Mx—overturning moment
My—acceleration and brake torque
Mz—steering moment
It has onboard conditioning and amplifiers to improve the signal-to-noise ratio.
Hardware Overview
18
SWIFT 30 Sensors
Construction
(Components exaggerated to show detail)
Slip
Ring
Slip Ring Bracket
(Spider)
Transducer
Interface
Cable
Anti-rotate Device
(Bend to fit vehicle)
Transducer
Customer-supplied
Attachment Bracket
Tire
Wheel Rim
Customer-supplied
Rim Adapter Flange
Hub
Adapter
Attach to
vehicle
suspension
S20-04
Hub adapter The hub adapter attaches to the inner diameter of the transducer, allowing you to
place it at the original position of the spindle face of the vehicle. The hub adapter enables you to maintain the original position of the tire on the vehicle while the transducer is attached to the vehicle (the tire will not protrude from the vehicle).
Components Set Up for Test Track
Slip ring bracket
(spider)
The slip ring bracket (also referred to as the “spider”) is used to attach the slip ring to the transducer. It has internal wiring that provides excitation power to the strain gage bridges and brings signals out from the transducer to the slip ring.
Encoder An encoder measures the angular position of the transducer. The SWIFT sensor
uses an optical encoder, integrated into the slip ring assembly, that counts off “ticks” to measure the angular position as the wheel rotates. It measures 2048 (512 plus quadrature) points per revolution (ppr) with a resolution of 0.18 degrees and an accuracy of 0.18 degrees.
Slip ring The slip ring allows you to output the transducer bridge signals and angular
position to the TI. A transducer data cable attaches from the slip ring to the back panel of the TI. The slip ring is not used for non-spinning applications.
Anti-rotate device The anti-rotate device is attached to the slip ring and the vehicle’s suspension (or
other non-rotating point). It is able to move up and down with the vehicle. Its primary function is to provide a fixed reference point for the optical encoder. Its secondary function is to prevent the cable from rotating with the wheel and becoming tangled or breaking.
The anti-rotate device is mainly used for road data collection. Although it can also be used for short periods of time on a road simulator. MTS does not recommend this use. Due to the extreme fatigue loading characteristics of durability testing on road simulators, we suggest that you either remove the slip ring assembly before installing the vehicle on a road simulator, or use it only for iteration passes, then promptly remove it.
SWIFT 30 Sensors Hardware Overview
19
Construction
Wheel Well
A jarring motion will damage the slip ring
Allow enough clearance for all loading and suspension travel
S20-05
Shunt B
Shunt A
Accelerometer
(optional)
Load
S30-25
Connector Housing
The anti-rotate device should be configured such that no loading occurs to the slip ring throughout all loading and suspension travel. This means that when you attach the anti-rotate device to the vehicle, you must consider all possible motion of the suspension. The anti-rotate device should not bump against the wheel well at any time; any jarring of the anti-rotate arm will damage the slip ring. For steering axles, the anti-rotate bracket must be mounted to part of the unsprung suspension that steers with the tire, such as the brake caliper. For additional anti­rotate device mounting recommendations, refer to the Anti-Rotate Customer/ User Assembly drawing at the back of this manual.
Non-spinning
connector housing
The non-spinning connector housing or the non-spinning connector bracket (both shown below) provide a connection between the SWIFT and the TI electronics for non-spinning use. Both assemblies incorporate rugged connectors suitable for durability testing. The non-spinning connector housing can also include an optional connector with built-in, tri-axial accelerometers.
Hardware Overview
20
SWIFT 30 Sensors
Construction
S30-26
Non-Spinning
Cable Assembly
Non-Spinning
Connector Bracket
Spinning
Slip Ring
Bracket
Non-Spinning
Connector Bracket
Transducer Interface
(TI)
Additional
components
The TI conditions the power supply, and uses previously stored calibration values to convert the eight bridge outputs and the encoder signal to six non-rotating analog outputs (Fx, Fy, Fz, Mx, My, Mz) plus an angle output. The force and moment outputs have a value of 10 V full scale, unless a different full-scale output is requested by a customer. The angle output is a 0–5 V sawtooth output.
Additional components that are supplied with your SWIFT sensor include shunt and transducer data cables, TI power cable, a SWIFT Transducer Interface Utilities disk, and the calibration file. MTS can also provide a 12 V DC power converter for use in the test laboratory.
SWIFT 30 Sensors Hardware Overview
21
Construction

Design Features

Flexure isolation The SWIFT sensor has a very stiff outer ring and flexured beam isolation which
render it relatively insensitive to stiffness variations in matings with rims and road simulator fixtures.
Flexure isolation minimizes thermal expansion stresses. With flexure isolation, if the inner hub experiences thermal expansion the beams are allowed to expand out, resulting in lower compressive stress on the beams.
Thermal stability The entire sensor is machined from a solid, specially forged billet of high
strength aluminum or titanium. The absence of bolted joints permits an efficient transfer of heat across the sensor structure, minimizing temperature differentials in the gaged area.
As mentioned earlier, flexure isolation allows thermal expansion with minimal stresses.
The transducer is designed to accommodate the high temperature environments that occur during severe driving and braking events. Individual temperature compensation of each strain gage bridge minimize temperature induced variations in accuracy. Since minimal electronics reside on the SWIFT sensor, it can easily tolerate high temperatures. The temperature rating for the SWIFT sensor is 125° C (257° F) at the spindle hub.
Temperature compensation is done on each bridge for better performance in transient or non-uniform temperature occurrences.
Low hysteresis The SWIFT sensor has very low hysteresis, since the sensing structure is
constructed with no bolted joints. Micro slippage in bolted joints contributes most of the hysteresis in highly stressed structures. Hysteresis errors due to micro-slip at joints can contribute to unresolvable compounding errors in coordinate transformation of the rotating sensor.
Low noise The SWIFT sensor uses a slip ring rather than telemetry for the transducer output
signals. On-board amplification of the transducer bridges minimizes any slip ring noise contribution.
Low cross talk The advanced design of the SWIFT sensor means that it has very low cross talk.
The alignment of the sensing element is precision machined. This alignment is critical to achieving minimum cross talk error between axes and minimum errors in coordinate transformation (from a rotating to a non rotating coordinate system). Any small amount of cross talk present is compensated by the TI.
Velocity information Angular output is available from the TI when it is used in the spinning mode with
the encoder. This angular output can be used to calculate wheel velocity. In non­spinning applications, accelerometers can be integrated into the transducer connector housing.
MTS does not supply any conditioning electronics for accelerometers. Ask your MTS consultant for more information about this option.
Hardware Overview
22
SWIFT 30 Sensors

Coordinate System

Fx
Fy
Fz
Mz
Mx
My
Transducer
Interface
Output signals
+
10 Volts
Angular Position
Bridge
Outputs
S20-06
+Mz
+Fz
+Fy
+My
+Mx
+Fx
Forces acting on outer ring
S20-07
In the transducer, independent strain gage bridges measure forces and moments about three orthogonal axes. The signals are amplified to reduce the signal-to­noise ratio. An encoder signal indicates angular position, which is used to convert raw force and moment data from the rotating transducer to a vehicle­based coordinate system. The force and moment and encoder information is sent to the transducer interface (TI).
Coordinate System
The TI performs cross talk compensation and converts the rotating force and moment data to a vehicle coordinate system. The result is six forces and moments that are measured at the spindle: Fx, Fy, Fz, Mx, My, and Mz. A seventh (angular) output is available for tire uniformity information, angular position, or to determine wheel speed (depending on the data acquisition configuration).
The coordinate system shown below was originally loaded into the TI settings by MTS. It uses the right-hand rule.
SWIFT 30 Sensors Hardware Overview
23
Coordinate System
The SWIFT coordinate system is transducer-based, with the origin located at the center of the transducer. Positive loads are defined as applied to the outer ring of the transducer.
Vertical force (Fz) is positive up
Lateral force (Fy) is positive out of the vehicle
Longitudinal force (Fx) is positive out of the transducer
You can change to the MTS Model 329 Road Simulator convention (lateral load into the vehicle is always positive) or to any coordinate system by changing the polarities in the calibration file. For instructions on how to change the coordinate system polarities, see the chapter, “Setting up the Transducer Interface.”
Hardware Overview
24
SWIFT 30 Sensors

Specifications

SWIFT 30 Transducer Performance
P
ARAMETER SPECIFICATION
Use
SWIFT 30 A (aluminum) for
SWIFT 30 T (titanium) for
Maximum usable rpm
Maximum speed
fits rim size (usable range)
Maximum hub bolt circle diameter accommodates M12 or 1/2 inch studs
Input voltage required
Input power required per transducer
Output voltage ± full scale calibrated load
SAE J328 rated load capacity
Standard Maximum Calibrated Load Rating‡
Longitudinal force (Fx)
Lateral force range (Fy)
Vertical force range (Fz)
Overturning moment (Mx)
Driving/braking moment (My)
Steering moment (Mz)
Resolution (analog system)
Noise level (peak-to-peak 0-500 Hz)
Performance accuracy
Nonlinearity
Hysteresis
Modulation§
Cross talk
Maximum operating temperature
Low level amplifiers
Transducer interface
#
6.5 kN (1,460 lbf) 10.7 kN (2,400 lbf)
±28 kN (±6,295 lbf) ±50 kN (±11,240 lbf)
±23 kN (±5,170 lbf) ±40 kN (±8,990 lbf)
±28 kN (±6,295 lbf) ±50 kN (±11,240 lbf)
±5 kN•m (±44,255 lbf•in) ±9 kN•m (±79,660 lbf•in)
±7.5 kN•m (±66,380 lbf•in) ±13 kN•m (±115,060 lbf•in)
±5 kN•m (±44,255 lbf•in) ±9 kN•m (±79,660 lbf•in)
Specifications
low weight, high sensitivity
high fatigue life, durability
2,200
240 kph (150 mph)
12–15 inch
*
120.65 mm (4.75 in)
10–17 VDC
30 W maximum (22 W typical)
±10 V
Aluminum Titanium
Infinite
15 N (3.4 lbf) 25 N (5.6 lbf)
1.0% full scale
0.5% full scale
3.0% reading
1.5% full scale
70°C (158°F)
50°C (122°F)
* A special flange configuration is required for a 12 inch wheel. Larger diameter rims can be used,
providing that overall clearance from brake calipers and suspension components is maintained.
† Load impedance >1 kΩ; 0.01 µF (maximum) load capacitance. ‡ The actual calibrated range may be different based on individual customer requirements. Consult the
calibration range sheet that accompanies each transducer for the correct calibration range.
§ Typical value on most steel rims. Aluminum rims typically have slightly higher modulation, but at a lower added weight.
# Each SWIFT sensor is calibrated on an MTS calibration machine. MTS provides complete documentation
of calibration values for each SWIFT unit
SWIFT 30 Sensors Hardware Overview
25
Specifications
Transducer Center-of-Gravity
Transducer Center-of-Gravity and Inertia Specifications
ATERIAL
M
ALUMINUM TITANIUM
Xcg 0.0 mm 0.0 in 0.0 mm 0.0 in
Ycg 26.3 mm 1.035 in 26.3 mm 1.035 in
Zcg 0.0 mm 0.0 in 0.0 mm 0.0 in
181 lb·in
94 lb·in
2
441 kg·cm2151 lb·in
2
854 kg·cm2292 lb·in
2
441 kg·cm2151 lb·in
Ixx
Iyy
Izz
274 kg·cm294 lb·in
530 kg·cm
274 kg·cm
2
2
Transducer Interface (part 1 of 2)
P
ARAMETER SPECIFICATION
Physical
Height
Width
Depth
Weight
Rack Mounting Kit
31.75 mm (1.25 in)
431.8 mm (17 in)
215.9 mm (8.5 in.)
1.68 kg (3 lb 11.1 oz)
Optional
2
2
2
*
Environmental
Ambient temperature
Relative humidity
Hardware Overview
26
0° C (32° F) to 50° C (122° F)
0 to 85%, non-condensing
SWIFT 30 Sensors
Transducer Interface (part 2 of 2)
P
ARAMETER SPECIFICATION
Power Requirements
Input voltage
Supply current
Fuse
Angular velocity
Encoder limit
Processing limit
Encoder resolution
10–17 V DC
2 A typical, 3 A maximum at 12 V DC
3 A fast-blow
2,200 rpm maximum
10,000 rpm maximum
2048 counts per revolution (512 pulses with quadrature)
Specifications
Time delay (encoder tick to main output stable)
Transducer cable length
Shunt cable length
Analog outputs
Vol tag e
12 µs (typical)
100 ft maximum
100 ft maximum
±10 V range† (force and moment outputs) 0–5 V sawtooth (angle output)
Capacitive load
Current
Noise at output, with typical gains
0.01 µF maximum
6 mA maximum
7 mVpp, DC - 500 Hz (typical) 15 mVpp, DC - 500 Hz (maximum)
Bandwidth (bridge input to main output)
–3 dB at 30.1 kHz (typical) 90 degree at 16.6 kHz (typical)
* Add 25.4 mm (1.0 in) for ground lugs. † Standard from MTS. Other full scale voltages can be evaluated and may be provided at special
request.
SWIFT 30 Sensors Hardware Overview
27
Specifications
Transducer Interface Communications
P
ARAMETER SPECIFICATION
Communications Channel # 1 (Remote Host Connections)
Baud rates
Parity
Stop bits
Data bits
Isolated RS-232/RS-485 interface power supply
Electrical interface
19,200 Kbits/s
None
1
8
+5 V DC @ 200 mA maximum
Isolated RS-232 or RS-485 remote host connection Isolated RS-485 TI to TI connection
Maximum number of devices that can be part of a RS-485 multidrop chain
Maximum cable length
32 with RS-232 remote host 31 with RS-485 remote host
*
For RS-232 host:
50 ft from host to the first (nearest) TI,
and
300 ft from the first TI to the last SWIFT TI in the RS­485 multidrop chain
For RS-485 host:
300 ft from host to the last (furthest) TI in the RS-485 multidrop chain
* Includes all compatible devices, such as an MTS 407 Controller. A maximum of only nine transducer
interfaces can be connected, because the addresses are limited to 1–9.
Hardware Overview
28
SWIFT 30 Sensors

Calibration

Calibration
Each transducer is calibrated by MTS before shipment. The transducer and TI may be returned to MTS for repair and recalibration as required.
Calibration is performed at MTS on a special fixture that is capable of applying multiple loads to the transducer. During calibration, raw signals are measured. The calibration gains and cross talk compensation values are computed from this raw data. These gains are recorded in a calibration file.
A unique calibration file is supplied for each transducer. The serial number of the TI associated with the transducer is listed at the top of the calibration file. A label with the serial number of the TI box (and the SWIFT sensor with which it was originally calibrated) is located at the back of each TI box.
The calibration file is loaded into the TI non-volatile RAM by MTS before the transducer is shipped. A copy of the file is also provided on a diskette.
MTS verifies the calibration by applying loads to the transducer, measuring the main outputs and checking for accuracy. Final calibration reports are provided with each transducer.
Shunt calibration At the end of the calibration process, a shunt calibration is performed. During a
shunt calibration, a resistance is introduced into the bridge circuit. The difference between the shunted and unshunted voltage is the delta shunt reference value for each bridge. That value is saved in the calibration file, which is downloaded from a PC or laptop computer and stored in non-volatile memory in the TI.
At any time afterward, pressing the Shunt button on the front of the TI causes each of the strain gage bridges to be shunted in sequence, and the measured shunt voltage (delta shunt measured value ) is compared to the reference value.
An acceptable tolerance range is also loaded into the TI memory during system calibration. One tolerance value is used for all bridges. This value is loaded as a percentage of allowable deviation from the delta shunt values. For example, if the FX1 bridge has a shunt delta reference value of –3.93, and the tolerance is set at 2 (percent), the acceptable range for the measured value would be –3.85 to –4.01.
SWIFT 30 Sensors Hardware Overview
29
Calibration
When you press the Shunt button, the associated Shunt LED lights. As the TI automatically switches through the series of bridges, it verifies that the outputs are within the accepted tolerance range. If all bridge shunt values fall within the tolerance range, the Shunt LED on the front panel will go off (after several seconds). If any bridge fails to fall within the shunt tolerance range, the LED will blink, indicating that the shunt calibration has failed. See the chapter,
“Troubleshooting,” on page 127, for more information on dealing with shunt
calibration failures.
ShuntTolerance=2 FX1ShuntDeltaRef=-3.91836 FX2ShuntDeltaRef=-3.91896 FY1ShuntDeltaRef=-3.92366 FY2ShuntDeltaRef=-3.91639 FY3ShuntDeltaRef=-3.91824 FY4ShuntDeltaRef=-3.92494 FZ1ShuntDeltaRef=-3.92282 FZ2ShuntDeltaRef=-3.92673 FX1ShuntDeltaMeas=-3.91854 FX2ShuntDeltaMeas=-3.9192 FY1ShuntDeltaMeas=-3.92412 FY2ShuntDeltaMeas=-3.91572 FY3ShuntDeltaMeas=-3.91815 FY4ShuntDeltaMeas=-3.92464 FZ1ShuntDeltaMeas=-3.9227 FZ2ShuntDeltaMeas=-3.92646
Checking the
calibration
Example of Calibration File Shunt Data
The above example shows shunt data from the calibration file. This data may be transferred, using the TIXFER program, from the transducer interface RAM to a computer or from a computer to the transducer interface RAM. Note that items marked ShuntDeltaMeas are uploaded from RAM, but not downloaded from the computer. (For more information on TIXFER, see the chapter, “Software Utilities.”
You can check the calibration of a transducer at any time by pressing the Shunt switch. Subsequent shunt commands compare the current feedback values against those stored in the TI. You may set the tolerance values for each TI by editing the calibration file (see the chapter, “Setting up the Transducer Interface”, for instructions).
If the current feedback values from a shunt calibration are outside the tolerance, the Shunt LED blinks to indicate a failure.
Hardware Overview
30
SWIFT 30 Sensors

Transducer Interface

Fx
Fy
Fz
Mz
Mx
My
Transducer
Interface
Output signals
(± 10 Volts)
Angular Position
Bridge
Outputs
Transducer bridge output
signals and encoder
angular position signal are
sent through slip ring
Transducer Interface
converts signals to non­spinning vehicle coordinates, applies calibration gains and
cross talk compensation
Force, moment, and
angle analog signals
are output from
Transducer Interface
q
Angle signal
(05 Volts)
S20-08
The TI performs cross talk compensation, transforms the loads from a rotating to a non-rotating coordinate system, and produces an analog output signal suitable for any data recorder.
Transducer Interface
SWIFT 30 Sensors Hardware Overview
Cross talk
compensation
Cross talk occurs when a force is applied to one axis, but a non-real force is measured on another axis. The SWIFT sensor design has very low inherent cross talk. The TI compensates for any cross talk by subtracting the non-real forces when the amount of cross talk is known.
The amount of known cross talk is determined during the calibration process. Cross talk values will vary slightly for different rims. For example, a steel rim will have slightly different cross talk errors than a less rigid aluminum rim.
Signal conditioning The TI is specifically designed to be used for both spinning and non-spinning
applications. The TI performs signal conditioning and communications functions. The output from the TI is a high-level signal suitable for input into a multichannel data recorder or an MTS Automated Site Controller (ASC).
31
Transducer Interface
Fx1 Fx2 Fy1 Fy2 Fy3
Fy4 Fz1 Fz2
Fx Fy Fz Mx My
Mz
Geometric
Matrix
Zero and
Scaling
q
Cross
Coupling
Matrix
Rotational
Transformation
q
Inputs Outputs
Transducer Interface Functions
S20-09
The TI transforms eight inputs (amplified bridge signals) into three forces and three moments by the following process:
Applying a zero offset and scaling the signals
Using a geometric matrix to transform the signals into three forces and three
moments in the transducer reference frame
Using a cross-coupling matrix calculation to scale and sum the individual
signals into each output
In spinning applications, using a rotational transformation to put the forces
and moments into a stationary reference frame
The TI conditions the transducer signals, producing seven analog output signals proportional to the following values:
Longitudinal force (Fx)
Lateral force (Fy)
Vertical force (Fz)
Overturning moment (Mx)
Driving/Braking moment (My)
Steering moment (Mz)
Angle output (θ)
Analog signals The force and moment signals are output from the TI in the form of ±10 V
scale analog signals. These signals can be used by any data acquisition system.
The angle output is an analog voltage that is proportional to angular position. At 0° the output is 0 V. At 360°, the output is 5 V.
1
full
32
Hardware Overview
1. Standard from MTS. Other full-scale output voltages can be evaluated and may be
provided at special request.
SWIFT 30 Sensors
Transducer Interface
0 360°
5V
360°
q
Angle
Output
1 rev = 360°
S20-10
The angle output for a tire rotating at constant velocity can be represented by the following illustration:
Although you may not routinely use it, the angle output information is available for tasks such as tire uniformity testing and troubleshooting. You may also calculate angular velocity by measuring the frequency of the angle output signal.
Communications The TI provides a serial port for remote communication. The port allows
connection to an RS-232 or RS-485 host for multidrop communication. This interface is compatible with the MTS 407 Controller protocol, and 407 Controllers may also be in the same multidrop communication chain. A multidrop configuration can include up to 32 total devices in any combination, with a maximum of nine TIs (limited to addresses 1 through 9).
The serial interface provides the following capabilities:
allows the user to save and restore TI setup parameters.
is compatible with LabVIEW®.
is compatible with serial port-equipped computers (UNIX machines,
Macintosh, and IBM PC).
is able to link multiple TIs (and 407 Controllers) to one host computer.
SWIFT 30 Sensors Hardware Overview
33
Transducer Interface
S20-11
Fuse
Power Switch
and Indicator
Shunt Switch and Indicator
Angle Zero
Switch and Indicator
Bridge Zero
Switch and Indicator
Fail
Indicator
Transmit Indicator
Address Selector

TI Front Panel

Fuse (F1) A 3A fuse protects the electronics.
Transducer Interface Front Panel
Power switch and
Indicator
The power switch turns power on and off. A green indicator will light to indicate that the TI power is turned on.
Shunt switch Pressing this switch performs a shunt calibration (shunt cal) of the transducer.
You do not need to hold the switch in continuously, only until the Shunt indicator lights up (indicating that the TI has started the shunt cal).
Before you perform a shunt cal, check that the appropriate shunt reference value and error tolerance have been downloaded (these values are normally loaded during system calibration, and are referred to as the shunt delta cal values).
A shunt calibration will determine the current delta values by measuring the bridges unshunted and shunted, and then compare these values to the previously loaded calibration values. If the measured values are outside of an acceptable tolerance, the Shunt indicator will flash, indicating an error.
Shunt Indicator This indicator indicates the current state of the shunts. If there are any active
shunts, or if you are currently performing a shunt calibration, this indicator will be lit.
If the shunt cal check fails, this indicator flashes (at approximately a 1 Hz rate).
Note The state of the shunt cal check is cleared at power-up, so the shunt cal
should be performed when the system installation is in question.
Hardware Overview
34
SWIFT 30 Sensors
Transducer Interface
[SWIFT] Name=zero 3 after new tire SerialNum=1234567 Normalization=0 InputSwitches=255 OutputPolarities=40 ZeroAlgorithm=3 AngleMode=0 AngleOffset=82.0898 AngleFixed=0 ZFX1=0.103786 ZFX2=-0.023199 ZFY1=-0.094017
Angle Zero and Bridge
Zero switches
These switches are used to zero the transducer inputs. Which switch you press depends on the ZeroAlgorithm that you specified in the calibration file (see following illustration). Two different methods are used to zero the system: spinning and non-spinning. For more detailed information on selecting a zero method, see the chapter, “Setting up the Transducer Interface.”
When you select a zero method, it will activate the appropriate switch on the TI front panel. Each switch performs a specific zero function:
Angle Zero– Angle offsets are required for spinning applications only. This switch is active when the ZeroAlgorithm=1, or 3. The TI reads the current angle and compensates for any offset from the Z axis facing up. You will not use this switch for non-spinning applications.
Bridge Zero–Bridge offsets are required for both spinning and non-spinning applications. This switch is active when the ZeroAlgorithm=0, 1, or 3. The TI reads the transducer bridge values and compensates for any offsets so that the bridge output is 0 at 0.0V.
SWIFT 30 Sensors Hardware Overview
35
Transducer Interface
When a system zero is initiated, the associated LED is lit. After successful completion of the system zero, the LED turns off. If there is a failure during the system zero, the LED will flash at approximately a 1 Hz rate.
Angle Zero and Bridge Zero Switch Functions
Z
ERO ALGORITHM WHEN TO USE ANGLE ZERO BRIDGE ZERO
0
(Preferred method for non-spinning applications)
1
Use this algorithm for non-spinning (fixed) applications.
Use this algorithm for spinning applications.
You will need to mechanically level the
The Angle Zero switch is non-functional.
Press the Angle Zero switch to read the current angle and use the value to set the angle sum to 0.0°.
Press the Bridge Zero switch to measure the static transducer bridge offsets.
Press the Bridge Zero switch to measure the static transducer bridge offsets.
SWIFT sensor.
3
Use this algorithm for spinning applications.
You do not need to mechanically level the
Both the Angle Zero and Bridge Zero switches are functional. This algorithm will perform both angle zero and bridge zero processes regardless of which button you press.
SWIFT sensor.
4
(Preferred method for spinning applications)
Use this algorithm for spinning applications.
You will need to
Both the Angle Zero and Bridge Zero switches are functional. This algorithm will perform both angle zero and bridge zero processes.
mechanically level the SWIFT sensor.
Hardware Overview
36
SWIFT 30 Sensors
Transducer Interface
Zero LEDs These indicators indicate the current state of the zero process. The
ZeroAlgorithm value (0, 1, 3, or 4) you selected in the calibration file will determine the state of the indicators when you press either the Bridge Zero or the Angle Zero button.
The indicators are off under normal operating conditions
In non-spinning applications using ZeroAlgorithm=0 (required), press the
Bridge Zero button. The Bridge Zero indicator will light for 3–4 seconds while the TI is completing the bridge zero process.
In spinning applications using ZeroAlgorithm=1 (alternate), pressing the
Bridge Zero button will light the Bridge Zero indicator continuously (no flashing) until the wheel is spun for one revolution (index-to-index). This may take up to two full revolutions, depending on where the encoder index pulse starts. After one revolution of data is collected, the Bridge Zero indicator will flash rapidly for 30 seconds while the data is analyzed and the bridge zeroes are calculated.
When you press the Angle Zero switch, the Angle Zero indicator will light for a few seconds while the TI reads the current angle and sets the angle offset value.
In spinning applications using ZeroAlgorithm=3 (alternate), both the
Bridge Zero and Angle Zero indicators will light continuously until the wheel is spun for one revolution (index-to-index). After one revolution of data is collected, both indicators will blink rapidly for approximately two minutes while the TI analyzes the data and calculates both the angle offset and bridge zero values.
In spinning applications using ZeroAlgorithm=4 (preferred), the Bridge
Zero and Angle Zero indicators will initially be off. After the wheel is turned at least 1.25 turns in order for the TI to locate the index, the level can be installed and leveled. When the Bridge Zero button is pressed, the Bridge Zero indicator will light continuously for a few seconds, then start blinking rapidly. The Angle Zero indicator will start blinking slowly.
When you press the Angle Zero button, the Angle Zero indicator will light continuously for a few seconds. Then both the Bridge Zero and Angle Zero indicators will turn off.
If the algorithm was unable to calculate zero, the Fail indicator will light momentarily and both the Bridge Zero and Angle Zero indicators will blink continuously at approximately a 1 Hz rate.
If no successful zero has been performed for the currently selected zero
algorithm, the Bridge Zero and Angle Zero indicators will flash (at approximately a 1 Hz rate), until a zero has been initiated. Use the TISTATUS utility for a detailed explanation of the problem.
After successful completion of a zero algorithm, the Bridge Zero and Angle Zero indicators turn off. Should the system zero fail, the indicators will return to a flashing state.
SWIFT 30 Sensors Hardware Overview
37
Transducer Interface
Address selector Each TI in a communications chain has a unique address. This address is used in
every read or write command from the host computer. The host can transmit to only one TI at a time, using its assigned address. The TI will reply to the host when it has received a command.
The address selector switch allows you to set the communication address for the TI. When multiple TIs are connected, each must have a unique address. The address must be 1 to 9. Address 0 is used only for broadcast messages from the host. In the case of broadcast messages, the TI does not respond to the host.
To change an address, insert a small screwdriver in the slot and turn the dial until the arrow points to the desired address number.
Note Make sure every TI on a communications chain has a unique address. If
you set two TIs on one communications chain to the same address, you may experience unpredictable communications errors.
If two TIs on one communications chain have the same address, communications to either TI will be unreliable. (The errors are unpredictable, but will probably be parity or framing errors.) Assigning the same address to two TIs does not damage the hardware.
Transmit Indicator The green Transmit indicator lights to indicate that the TI is transmitting
information via the COMM IN connector.
FAIL Indicator The red Fail indicator lights to indicate that a fail condition exists on the board.
Depending on the failure detected, the Fail indicator will either be on constantly or will flash a repetitive pattern that can be used to identify the failure detected.
Certain failures are considered critical, and will result in the TI becoming completely unusable. These failure conditions must be resolved before the TI can be used. If a critical failure occurs, the Fail indicator will only blink the cause of the first critical failure. This failure code will be repeated approximately every 1 second.
Non-critical failures indicate impaired system functionality, which, in most cases, can be corrected operationally from the communication interface. Non­critical failure codes are checked cyclically, so that multiple failure conditions can be communicated. Failure codes are indicated approximately every 1.5 seconds.
The following table lists fail conditions and the manner in which the Fail indicator indicates the failure.
Hardware Overview
38
SWIFT 30 Sensors
F
AIL INDICATOR STATE
[NUMBER OF BLINKS:]
Transducer Interface
Error Codes for the Fail Indicator (part 1 of 2)
ERROR
Off
Continuous On
Fast blinking
Fast varying blink
1
2
3
5
6
7
8
No error detected
Critical: Boot failure; bad code in boot block
Critical: Unanticipated exception prior to relocation of loader code
Critical: Unanticipated exception after relocation of loader code
Critical: SRAM failure
Critical: Local register failure
Critical: Boot block CRC failure
NVRAM error. An error was detected during the NVRAM self-test. This self-test is performed at every power-cycle, and verifies that the NVRAM checksum is valid, and also that the data stored is compatible with the current firmware version. A failure of this test will require an NVRAM Init command to be issued. Issuing this command will result in all stored settings being cleared.
Self-Test fail. A failure was detected during the commanded self-test (note that this is different than the power-up self-test). Further information can be obtained by reading the self-test error status.
Operational error. These errors are usually caused by issuing communication commands with invalid Command IDs, out-of-range data, invalid slot number, and so on. This error condition is cleared after the Fail indicator has indicated it.
Serial EEPROM Error. A checksum or version error was detected on the serial EEPROM data. This data stores normalization values.
9
10
11
12
13
14
15
16
17
AD Failure. An error (gain out of range or offset out of range) occurred on at least one A/D, when the A/D gains and offsets were set. The ability to perform a zero, self-test or shunt tests may be impaired in this state.
Issuing a Cal A/D command may clear this state.
Critical: Memory allocation failure
Critical: An unexpected interrupt occurred.
Communication Interface Init Error. An error occurred while attempting to initialize the communication interface. The communication interface may be unusable in this state.
TI Firmware Init Error. An error occurred while attempting to initialize the TI firmware. The communication interface may be unusable in this state.
Box ID Error. An error occurred while attempting to initialize the TI Box ID. The communication interface may be unusable in this state.
DAC Init Error. An error occurred while attempting to initialize the TI DACs. The functionality of the TI may be impaired in this state.
Switch Init Error. An error occurred while attempting to initialize the TI switches. The functionality of the TI may be impaired in this state.
Encoder Init Error. An error occurred while attempting to initialize the TI encoder interface. The functionality of the TI may be impaired in this state.
SWIFT 30 Sensors Hardware Overview
39
Transducer Interface
AIL INDICATOR STATE
F
[NUMBER OF BLINKS:]
18
Error Codes for the Fail Indicator (part 2 of 2)
ERROR
AD Init Error. An error occurred while attempting to initialize the TI A/Ds. The ability to perform a self-test, and/or shunt tests may be impaired in this state.
19
Shunt interface Init error. An error while attempting to initialize the shunt interface. The shunt interface may be unusable in this state.
Hardware Overview
40
SWIFT 30 Sensors
Transducer Interface
J2A Shunt A
and J2B Shunt B
J4 Output
Comm In and
Comm Out
J3 Power
Ground
Terminals
Transducer
Connector
S20-12

TI Rear Panel

Transducer Interface Rear Panel
J4 Output connector The J4 Output connector provides the conditioned sensor outputs that can be
connected to a data acquisition or test control system.
Transducer connector Connect the data cable from the transducer slip ring to the Transducer Connector.
J2A Shunt A J2B Shunt B
The J2 connectors are used for the shunt cables. The shunt cables are connected to the two 6-pin shunt cal connectors on the front of the transducer.
connectors
Comm In Comm In is an 8-pin modular phone jack connector (RJ-45) that provides a
connection to an RS-232/RS-485 remote host, or to another TI in an RS-485 multidrop communications chain. The cable connected to Comm In selects an RS-232 or RS-485 interface. The RS-232/RS-485 interfaces on Comm In are electrically isolated from the TI power. This connection is only needed when you are downloading new settings to the TI module.
Under normal operating conditions, no host connection is required. The Comm In and Comm Out connectors allow you to daisy-chain multiple boxes without Y cables or multiple connections to the host computer.
Comm Out Comm Out is an 8-pin modular phone jack connector (RJ-45) that provides a
connection to another TI chassis in an RS-485 multidrop communication chain.
J3 Power connector Connect a power cable from an external 12 V DC source.
Ground Terminals The ground terminals enable you to ground the TI, and chain several TI boxes
together.
SWIFT 30 Sensors Hardware Overview
41
Transducer Interface
X2
X1
X4
X5
X6
S20-13

TI Jumpers

J
UMPER SETTING FUNCTION
The transducer interface uses circuit board jumpers to establish certain parameters and make use of various electronic functions. These jumpers are set at the factory, and should not be reset. The following table is for reference only.
X1
1–2
2–3
X2
1–2
2–3
X4 removed
X5 installed
removed
X6 installed
removed
Excitation setup for shunts FX1, FY1, FY4, and FZ2.
Sets up – (minus) excitation for shunts FX1, FY1, FY4, and FZ2.
Sets up + (plus) excitation for shunts FX1, FY1, FY4, and FZ2.
Excitation setup for shunts FX2, FY2, FY43 and FZ1.
Sets up – (minus) excitation for shunts FX2, FY2, FY43 and FZ1.
Sets up + (plus) excitation for shunts FX2, FY2, FY43 and FZ1.
Not used for TI applications (Standard setting).
Enables the ability to download new code to the block of FLASH RAM where the boot code is stored.
Disables the ability to download new code to the block of FLASH RAM where the boot code is stored (Standard setting).
Boots to the FLASH memory down-loader.
Boots to the Transducer Interface software (Standard setting).
Hardware Overview
42
TI PWB Jumper Locations
SWIFT 30 Sensors

Interfacing with RPC

The SWIFT sensor is directly compatible with the MTS Remote Parameter Control (RPC) simulation software. The SWIFT system produces outputs that directly correspond to the uncoupled spindle forces that the MTS Model 329 Road Simulator applies to the vehicle. Traditional instrumentation techniques provide coupled suspension loads data. Using the SWIFT sensor, the RPC simulation software needs to apply less correction to obtain the road simulator drive signals. Fewer iterations are required to recreate the measured loads.
You must ensure that the full scale value for your data recorder and the MTS Series 498 electronics match. MTS electronics are typically set at ±10 V full scale, while some data recorders are ±5 V full scale.
The SWIFT sensor is calibrated for ±10 V full scale. To recompute the TI gains for ±5 V full scale, a verification pass must be run or the calibration will not be traceable. Upon special request, MTS can evaluate and may provide calibration for ±5 V or other full scale voltages.
Interfacing with RPC
SWIFT 30 Sensors Hardware Overview
43
Interfacing with RPC
Hardware Overview
44
SWIFT 30 Sensors

Software Utilities

Contents Introduction 46
TISTATUS - Transducer Interface Status 47
TIXFER - Transducer Interface Transfer 48
TISHUNT - Transducer Interface Shunt 50
Setting Up Shunt Calibration Reference Values 54
TISETZERO – Transducer Interface Set Zero Method 55
Error Messages 56
Shunt Error Status 57
SWIFT 30 Sensors Software Utilities
45

Introduction

Introduction
The SWIFT utility programs in this distribution are for Win32 Operating Systems (Windows 95, 98, NT, 2000, XP). They are designed to be run from the Command Prompt or MSDOS Shell. However, it is possible to create a shortcut to run the programs. If launched from a shortcut the application window may close immediately when the application terminates making it impossible to see any error messages. The Command Prompt application is usually found in Start–>Programs–>Accessories but the actual location depends on the version of your operating system.
To run a SWIFT utility program
Copy it to your computer. For example, create the folder
the executables (*.exe) to that folder.
Launch Command Prompt
Change the working directory to where you copied the executables: cd bin.
This step can be eliminated if you set up the PATH environment variable to
include the directory where you copied the SWIFT utility executables.
Type the name of a SWIFT utility program providing the necessary
command line arguments: provided the program will display a simple help message. This is helpful if you forget the order of the command line arguments.
In the Windows environment the SWIFT utilities programs define port 1 as COM1: and port 2 as COM2:. Which communications port you specify depends on which connector on the computer the serial communications cable is plugged into. To confuse things, some computers label the communications connectors as “A” and “B”.
1
tixfer 1. If no command line arguments are
C:\bin and drag
2
Software Utilities
46
1. You may want to change the layout properties for the Command Prompt window to display a larger area or to increase the screen buffer size. Within Command Prompt, select Properties and the Layout tab to modify the screen buffer size or window size.
2. In Windows 2000 the environment variables can be changed at
Start–>Control Panels–>Systems. Click on the Advanced tab, and the Environment Variables… button. The path is a system variable. Adding
;c:\bin, or whatever directory name you used, to the end of the string will
cause Command Prompt to search that directory for applications.
SWIFT 30 Sensors

TISTATUS - Transducer Interface Status

TISTATUS - Transducer Interface Status
This program is used to get status information from the SWIFT Transducer Interface (TI). When the TI has encountered a problem and is blinking an error code, this program can be used to easily interpret the error. For certain errors this program may provide additional information. The program also provides information such as the internal power supply voltages.
Note The power supply voltages displayed may be unreliable if the power
supplies are too low, as the circuit used to measure the power supply also depends on the available power.
Syntax The tistatus command requires two arguments:
tistatus port box
port is the communications serial port number
1 = COM1: 2 = COM2:
box is the TI communications address
1 = lowest possible address 9 = highest possible address
Example
C:\bin>tistatus 1 1
tistatus $Revision: 1.6 $ ($Date: 2002/04/10 21:05:49 $)
Reads status from the SWIFT Transducer Interface Requires that the remote comm port be configured for 19200 baud, 8 data bits, no parity, 1 stop bit.
Tue Dec 28 10:15:14 2004 Firmware Version: 2.6.1 Ground = 0 +5V Supply = 4.98904 +15V Supply = 14.9479
-15V Supply = -14.9433 +5V Ref = 5.00092
-5V Ref = -5.00763 No system errors to report Closing the communications port... Program completed.
SWIFT 30 Sensors Software Utilities
47

TIXFER - Transducer Interface Transfer

TIXFER - Transducer Interface Transfer
This program is used to change settings within the SWIFT Transducer Interface (TI). It can be used to read the current settings and save them to the computer (upload) or write the settings to a TI with values from a file on the computer (download).
Syntax The tixfer command requires one argument:
tixfer port
port is the serial port number
1 = COM1: 2 = COM2:
Example
C:\bin>tixfer 1
tixfer $Revision: 1.11 $ ($Date: 1999/04/21 10:12:40 $)
0...exit
1...Upload/Save a box
2...Restore/Download a box Enter choice? 1 Enter TI box address? 1 Enter output specifications filename? example.cal Enter description? example for uploading settings Allocating box... Initializing box...
File Format The file used with commands contains a header and a list of parameters.
Transducer calibrations can be uploaded and saved individually. If a test needs to be rerun at a later date but the original transducer is not available, another transducer can be used by downloading its calibration information.
The header must be the first thing in the file, and it must be in the form:
[SWIFT]
Following the header is a list of parameter settings. The syntax is:
ParamName=ParamValue
The following rules apply:
Tabs and spaces are allowed.
The parameters can occur in any order
Names are case insensitive. If a parameter name is not recognized, an error will be reported, and further processing will be stopped.
If an error causes the program to abort while downloading, any parameters prior to the error will have been successfully downloaded because parameters are downloaded as they are read.
Software Utilities
48
SWIFT 30 Sensors
TIXFER - Transducer Interface Transfer
CAUTION
CAUTION
Make important files read-only after uploading. After uploading important files, such as those containing calibration data, make them read-only.
If not protected, important data may get overwritten.
Make important files read-only, and make backups of important data.
Check force and moment output signals after downloading new settings.
Downloading new settings may affect Transducer Interface outputs.
After downloading new settings, force and moment output signals should be monitored to check basic system operation.
More about TIXFER
files
The files created by TIXFER are plain text files that can be read by Microsoft Notepad or WordPad. In general, use a common extension such as “.cal” to help identify the files, but that is not required. The settings files contain both configuration settings and calibration settings. As a general rule parameters that begin with K are calibration gains and should not be edited. Configuration settings such as the zero algorithm can be changed without affecting the calibration.
Whenever downloading settings, make sure the file is for the transducer connected to the SWIFT Transducer Interface. Usually the filename for the settings contains the serial number for the transducer. If settings for one transducer are used with another they will not be accurate. Because the TI is calibrated by itself, calibration settings for a given transducer can be used with any TI, however, some calibration methodologies require the transducer, cable and TI to be used as a calibration set (end-to-end calibration).
The serial number in the TIXFER settings file is the serial number of the TI that the settings were first uploaded from.
The bridge and angle zero values will change whenever a zero is activated by pressing the TI front panel zero button. Therefore, after a zero is performed the zero values uploaded will not match those downloaded.
All parameters within the TI have been calibrated. Because the resolution of each adjustable parameter is finite, downloaded values may vary slightly from subsequent uploads and the values uploaded from various units may be different. The downloaded value gets “snapped” to the closest realizable value. The realizable values depend on the resolution and calibration data for the parameter. Normally the gains from the SWIFT automated calibration stand are computed to a higher resolution than the TI is capable of dealing with.
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49

TISHUNT - Transducer Interface Shunt

TISHUNT - Transducer Interface Shunt
This program is a utility with various functions related to shunts. The SWIFT system includes the ability to connect a shunt resistor across each of the resistive bridges in the transducer. This shunt function can be used as a simple verification that the SWIFT system is working normally. Shunt verification activates the shunts and compares the results to those recorded during calibration. While this does not guarantee the transducer is still in calibration, it provides some level of confidence it is working normally. If the shunt results differ significantly from those recorded during calibration the SWIFT system should be evaluated for possible problems.
Syntax The tishunt command requires one argument, as follows:
tishunt port box
port is the communications
1 = COM1:
2 = COM2:
Example
box is the SWIFT-TI communications address
1 = lowest possible address
9 = highest possible address
Initializing box...SWIFT TI Shunt Main Menu
0...exit
1...Read current Shunt values
2...Set the TI shunt tolerance
3...Restore Shunt parameters from a file
4...Scan inputs & outputs with shunts
5...Command a shunt cal
6...Write last shunt measurements to a parameter file
Enter choice:
The Shunt Main Menu options are described in the following paragraphs.
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50
SWIFT 30 Sensors
TISHUNT - Transducer Interface Shunt
Option 0 Use this option to exit the program.
Option 1 Use this option to read the shunt tolerance, the last measured shunt values, the
reference values, and the shunt error status.
Note The shunt error status is not maintained over power cycles, so it is only
valid if the shunt is executed after power is applied. Refer to, “Shunt
Error Status,” on page 57.
This option asks if you want to save the data in a file. Answer Y or N, and if Y, then supply the file name when prompted. The following is typical of what is displayed when this selection is made:
Reading Shunt parameters from TI... OK
Shunt Delta Tol: 10.000%
FX1 Ref: 3.935 Measured: 3.934 Error Status: 0
FX2 Ref: 3.932 Measured: 3.932 Error Status: 0
FY1 Ref: 3.937 Measured: 3.930 Error Status: 0
FY2 Ref: 3.929 Measured: 3.930 Error Status: 0
FY3 Ref: 3.932 Measured: 3.932 Error Status: 0
FY4 Ref: 3.931 Measured: 3.932 Error Status: 0
FZ1 Ref: 3.930 Measured: 3.935 Error Status: 0
FZ2 Ref: 3.932 Measured: 3.934 Error Status: 0
Save to a file (y/n)?
Note If you save to a file, the file is created in the same directory as the tishunt
program. The file name must contain less than 80 characters.
Option 2 Use this to set the shunt tolerance. When selected, the following is displayed:
The Shunt Tolerance specifies how much the measured shunt deltas may deviate from the Ref settings, and still be considered good.
The value is entered as a percentage, where "1.0" would mean 1.0% of the Ref settings.
For example: if the tolerance is 1%, and the Ref setting is 8.0, then the measured delta must be between 7.92 and 8.08 to be considered good.
It is not necessary to reboot the TI when this value is changed, but a Shunt Calibration must be executed to update the Shunt Error Status words.
Also note that a parameter download will overwrite this value.
Enter tolerance (in percent):
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51
TISHUNT - Transducer Interface Shunt
Option 3 Use this option to restore shunt settings from a file. The file format is the same as
that used in the tixfer program.
Option 4 Use this option to apply a shunt sequentially, reading the eight bridges and six
outputs of the Transducer Interface. Note that this option does not update the shunt measured values or error status. A reading is first made with no shunts applied (displayed as the zeroes data). The remainder of the readings are displayed as delta values from the original readings.
Enter Filename to save data to (the file will be appended): Enter Description: Reading bridges & outputs unshunted
FX1
FX
zeroes:
bridges: 0.000 0.002 0.000 0.000 0.001 0.000 0.001 0.000
outputs: -0.003 -0.006 0.001 0.000 -0.002 0.000
deltas:
Shunting FX1
bridges: -3.933 0.000 -0.001 0.002 -0.001 0.001 0.000 0.000
outputs: -9.014 0.031 -0.031 -0.001 -3.246 -0.188
Shunting FX2
bridges: -0.002 -3.929 0.000 0.001 0.000 0.001 0.001 0.001
outputs: -9.198 -0.049 0.026 -0.011 3.259 -0.072
Shunting FY1
bridges: -0.001 0.001 -3.931 0.001 -0.001 0.000 -0.001 0.001
outputs: 0.029 -8.493 -0.145 -3.695 0.024 0.002
Shunting FY2
bridges: 0.000 -0.001 -0.001 -3.930 0.000 0.000 0.000 0.001
outputs: 0.175 -8.322 0.031 0.021 -0.014 -3.647
Shunting FY3
bridges: -0.001 0.001 -0.001 0.000 -3.931 0.001 0.000 -0.001
outputs: 0.005 -8.538 0.163 3.692 -0.016 -0.003
Shunting FY4
bridges: -0.002 0.001 0.000 0.000 0.001 -3.932 -0.001 0.000
outputs: -0.150 -8.271 -0.018 -0.021 0.021 3.712
Shunting FZ1
bridges: 0.000 0.001 0.000 0.000 -0.001 0.002 -3.922 -0.001
outputs: 0.105 -0.010 -7.482 0.129 -2.892 -0.052
Shunting FZ2
bridges: 0.000 -0.001 0.000 0.001 0.000 0.001 -0.001 -3.931
outputs: -0.052 -0.081 -7.021 0.114 2.749 0.049
FX2
FY
FY1
FZ
FY2
MX
FY3
MY
FY4
MZ
FZ1 FZ2
Software Utilities
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SWIFT 30 Sensors
TISHUNT - Transducer Interface Shunt
Option 5 Use this option to command a Shunt Cal in the Transducer Interface. This is the
same as pressing the Shunt button on the front panel of the TI. A period is displayed on the screen for every change in the shunt state. This gives you a quick view of the progress.
TI Shunt Cal state 2 TI Shunt Cal state 5 TI Shunt Cal state 7 TI Shunt Cal state 8 TI Shunt Cal state 11 TI Shunt Cal state 14 TI Shunt Cal state 17 TI Shunt Cal state 20 TI Shunt Cal state 23 TI Shunt Cal state 26 TI Shunt Cal state 29 TI Shunt Cal state 32 TI Shunt Cal state 34 TI Shunt Cal state 35 TI Shunt Cal state 38 TI Shunt Cal state 41 TI Shunt Cal state 43 TI Shunt Cal state 44 TI Shunt Cal state 47 TI Shunt Cal state 0 TI Shunt Cal completed. Read results by selecting appropriate menu option.
Option 6 A valid shunt calibration should be performed prior to executing this command.
This option allows an easy means of setting the Shunt Calibration Reference values after calibration. After this option has executed, the file that was written can then be downloaded (using option 3). Downloading the file will set the Shunt Reference values to the last measured values, so that subsequent Shunt Calibrations should pass when the SWIFT system is setup properly, and fail when not setup properly.
Note This menu choice should only be used by qualified service personnel.
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TISHUNT - Transducer Interface Shunt

Setting Up Shunt Calibration Reference Values

The tishunt utility provides all of the necessary functions for setting up a Transducer Interface with valid Shunt Cal Reference values.
Note This procedure should only be performed by qualified service personnel.
Before running the tishunt utility, connect the Transducer cable and Shunt cables from the SWIFT TI to the SWIFT Transducer Assembly. Power up the SWIFT TI and wait for the red Fail indicator on the TI front panel to go out (this indicates that the TI is ready).
Note that it is not necessary to perform a System (Transducer) Zero prior to the Shunt Cal.
Procedure 1. Launch the tishunt utility.
2. Using Option 2, enter the desired shunt tolerance.
3. Using Option 5, command a shunt cal, and wait for it to complete. This causes the TI to apply and measure each shunt delta. These measured values will be written as the Cal Reference values. The Shunt indicator on the TI front panel should not blink (blinking indicates that the shunt cal verification failed).
4. Using Option 1, read the current shunt parameters. It is not necessary to save these to a file. Review the measured values and verify that they are correct.
5. Using Option 6, write the last shunt measurements to a parameter file. This sets up a file that contains the eight Set Shunt Cal Reference commands, with the last measured values as the values for the commands. This step does not download the values, but forces the generation of a shunt cal reference parameter file.
Write down the filename that is generated, as it will be required later.
6. Using Option 3, restore shunt parameters from a file. Enter the filename used in Option 6 (Step 5). The tishunt utility then downloads the shunt cal reference values to the TI. These values are written into non-volatile memory within the TI, and are automatically restored whenever the TI is powered up.
7. Using Option 5, command another shunt cal, and wait for it to complete. This provides a verification, showing that the values downloaded are valid.
The Shunt indicator on the TI Front Panel should not blink (blinking indicates that the shunt cal verification failed).
Software Utilities
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SWIFT 30 Sensors

TISETZERO – Transducer Interface Set Zero Method

TISETZERO – Transducer Interface Set Zero Method
This program allows some configuration settings to be changed in a SWIFT Transducer Interface (TI) without modifying a settings file. This program only changes configuration settings, it does not change any calibration settings.
Syntax :
tisetzero port box [zero_algo]
port is the communications
1 = COM1: 2 = COM2:
box is the TI communications address
1 = lowest possible address 9 = highest possible address
zero_algo is optional and specifies the zero algorithm
0 = lowest 4 = highest
Example
C:\bin>tisetzero 1 1
Firmware Version: 2.6.1 Current angle mode is ENCODER Current zero algorithm is SPINNING BRIDGE AND ANGLE UNLOADED Zero algorithms...
0) exit
1) fixed
2) spinning bridge
3) spinning bridge and angle unloaded
4) spinning 2 point
Enter choice?
Option 0
Use this option to exit the program
Option 1 Use this option for fixed (non-spinning) applications. It sets the AngleMode to 1
(fixed) and the ZeroAlgorithm to 0 (fixed). You may need to set the fixed angle manually.
Option 2 Use this option for spinning applications. It sets the AngleMode to 0 (encoder)
and the ZeroAlgorithm to 1 (spinning bridge, angle with level).
Option 3 Use this option for spinning applications. It sets the AngleMode to 0 (encoder)
and the ZeroAlgorithm to 3 (spinning bridge and angle)
Option 4 Use this option for spinning applications. It sets the AngleMode to 0 (encoder)
and the ZeroAlgorithm to 4 (2-point bridge and angle with level).
SWIFT 30 Sensors Software Utilities
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Error Messages

Error Messages
When a SWIFT utility encounters an error, a traceback message is displayed. An example traceback message is:
serial port command timeout, received: 0 chars, buffer:
-1: (DoTIUploadBox) upload box error
-1: (SwiftTI::Init) error reading typeid
-1: (MParm::ReadVal) error read value for Type ID
-1: (MPort::DoCommand) error sending or receiving response
-4: (MPort::GetResponse) error parsing error code
-4: (ParseErrorCode) expected @
Usually you only need to be concerned with the first line of the traceback which gives a summary of the error. The indented list of messages may provide additional information that in some instances will be helpful to determine the cause of an error. For instance, if the program reported an “out of range” error one of the other lines may indicate the name of the parameter being written to when the error occurred.
The number at the beginning of an indented error line is an error number. Negative error numbers are generated by the SWIFT utility program. Positive error numbers are generated by the TI.
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SWIFT 30 Sensors

Shunt Error Status

This is the error status for each bridge from the last shunt cal that was performed. The error status is a bit-mapped status word, where the error is present if the bit is set to 1.
Bit 0 = Bridge amplifier was saturated prior to applying the shunt.
Bit 1 = Bridge amplifier was saturated after applying the shunt.
Bit 2 = Measured delta value failed high.
Bit 3 = Measured delta value failed low.
Bit 4 = A procedural error occurred (unable to read a value, etc.).
In the following example the error status received is 5 indicating that bits 0 and 2 were set.
Bit 4 3210
Shunt Error Status
Bit Value168421
Example0 0101
Error Status=
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Shunt Error Status
Software Utilities
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SWIFT 30 Sensors

Setting up the Transducer Interface

Overview Two different software configurations are used by the TI, depending on whether
you will be using the SWIFT sensor on the test track (spinning application) or in the laboratory (non-spinning application). Angular transformation is required on the test track only. If you are using the same transducer and TI for data collection and simulation testing, you must change the software configuration before the TI can be used for simulation testing.
Contents Select a Zero Method 60
Calibration File Elements 61
Zero Algorithms 62
Upload the Calibration File 64
Edit the Calibration File 66
Download the Calibration File 70
SWIFT 30 Sensors Setting up the Transducer Interface
59

Select a Zero Method

Select a Zero Method
Before you install a transducer and zero it, you must configure the transducer interface (TI) for the appropriate zero method.
Equipment required You will need:
A laptop computer (at test track) or desktop PC
Serial port communication cable
SWIFT Transducer Interface Utilities diskette
Know the address assigned to each TI box
Some experience with DOS commands and text editors
Zero methods There are two separate zero algorithm classes used to zero the transducer inputs.
The method you choose depends on whether you will use the transducer in a spinning (test track) application (Zero Algorithm 1, 3 or 4) or non-spinning (road simulator) application (Zero Algorithm 0).
If you are using the same transducer with a road simulator that you used previously on the test track, you must re-zero the transducer using the non­spinning zero algorithm.
When you select an algorithm, you are also enabling the zero button(s) on the front panel of the TI. There are two zero buttons:
Bridge Zero
Angle Zero
What you need to do To change the zero algorithm used by the TI you will need to:
1. Copy the original calibration file from the diskette that came with the transducer to the computer.
2. Edit the calibration file to select a zero algorithm and angle mode.
3. Download the modified calibration file from the computer to the TI box.
4. Repeat the process for all of the transducers.
These steps are described in detail in the following sections.
Setting up the Transducer Interface
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SWIFT 30 Sensors

Calibration File Elements

[SWIFT] Name=zero 3 after new tire SerialNum=1234567 Normalization=0 InputSwitches=255 OutputPolarities=40 ZeroAlgorithm=4 AngleMode=0 AngleOffset=82.0898 AngleFixed=0 EncoderSize=0 ZFX1=0.103786 ZFX2=-0.023199 ZFY1=-0.094017 ZFY2=-0.184371 ZFY3=-0.225885 ZFY4=-0.269841 ZFZ1=-0.101343 ZFZ2=-0.045177 KFX1=0.196337 KFX2=0.195604 KFY1=0.169231 KFY2=0.166789 KFY3=0.167277 KFY4=0.16801 KFZ1=0.195849 KFZ2=0.196581 KMX=3.7558 KMYX=2.39805 KMYZ=2.5641 KMZ=3.75824 KFXFY=0.000611 KFXFZ=-0.00315 KFXMX=0.008864 KFXMY=-0.005348
SWIFT file identifier
Description of the file
Serial number of the Transducer Interface (TI)
Internal calibration for the TI
Polarity of the six outputs
(default = 40)
Zero Algorithm
Angle Mode
Angle Offset
Fixed Angle
Bridge Zeroes
Do Not Modify
Calibration Gains
Do Not Modify
Setting for all input switches
(default = 255, all closed)
S20-33
Encoder Size
The following figure shows some elements of the calibration file:
Select a Zero Method
SWIFT 30 Sensors Setting up the Transducer Interface
Items you may edit OutputPolarities—defines the polarities of the six outputs. Change these
ZeroAlgorithm—selects a zero algorithm for the application.
AngleMode—selects the mode used for determining the encoder sine and
AngleFixed—used for non-spinning applications.
AngleOffset— used for spinning applications. Normally you do not need to
EncoderSize
Typical Calibration File
only if your application requires different polarities from those on the transducer label.
cosine.
change this value.
depending on whether the application is using telemetry (0) or spinning slip
1
–defines the size of the encoder. The value will vary
ring (1).
1. Some older versions of TI electronics may have firmware versions that are not compatible with this parameter. If you are not using telemetry, this will not affect the function of the SWIFT. To allow proper function, load a current version of TIXFER or delete this line from the calibration file.
61
Select a Zero Method

Zero Algorithms

The following table lists the different values available and the angle zero and bridge zero functions that they perform:
Zero Algorithm Values Defined (part 1 of 2)
ERO ALGORITHM WHEN TO USE BRIDGE ZERO ANGLE ZERO
Z
0
1
Use this algorithm for non-spinning (road simulator) applications.
(AngleMode=1)
Use this algorithm for spinning (test track) applications.
You will need to mechanically level the SWIFT sensor.
The transducer is unloaded during the zero process.
(AngleMode=0)
When you press the Bridge Zero button, the TI measures the static transducer bridge offsets. It sets up zero DACs to provide 0.0 V raw bridge output.
The Bridge Zero LED will light for 3–4 seconds, and will go off when the zero process is complete.
When you press the Bridge Zero button, the TI will collect one revolution of raw bridge data, average the data, and remove the DC offset by setting the zero DACs to the average value.
The Bridge Zero LED will light continuously until the wheel is turned for one revolution (index-to-index). After one revolution of data is collect, it will flash (at approximately 4 Hz) for 30 seconds while the bridge zero values are computed.
The Angle Zero button is non­functional.
When you press the Angle Zero button, the TI will read the current angle and use the value to set the angle sum to 0.0 degrees.
The Angle Zero LED will light for a few seconds while the TI sets the angle offset value.
If you do not press the Angle Zero button, the value for AngleOffset will not be updated in the calibration file.
The wheel must be rotated past the encoder index pulse at least once after power up so that the electronics can determine the absolute angular position.
2
Setting up the Transducer Interface
62
Reserved for future use. N/A N/A
SWIFT 30 Sensors
Zero Algorithm Values Defined (part 2 of 2)
Z
ERO ALGORITHM WHEN TO USE BRIDGE ZERO ANGLE ZERO
Select a Zero Method
3
Use this algorithm if you do not need to mechanically level the
Both the Angle Zero and Bridge Zero buttons are functional. This algorithm will perform both angle zero and bridge zero processes.
SWIFT sensor
The transducer is unloaded during the zero process.
(AngleMode=0)
In the Bridge Zero process, the TI will average the data and remove the DC offset by setting the zero DACs to the average value.
In the Angle Zero process, the TI will collect one revolution of raw bridge data, perform a peak/valley analysis via sine curve fit for X1, X2, Z1, Z2, and determine the angle that will result in positive Z facing upward.
This process assumes that the wheel is hanging, so that the peak vehicle Z axis is read 180° out of phase (transducer peaks are the weight of the wheel, in a downward direction). The angle determined is then shifted by 180°.
4
This is the recommended algorithm for spinning
Both the Angle Zero and Bridge Zero buttons are functional. This algorithm will perform both angle zero and bridge zero processes.
applications.
The Bridge Zero button is pressed when the Z beam is facing up. You will need to mechanically level the SWIFT sensor
The Angle Zero button is pressed after the sensor is rotated 90° in
either the plus or minus direction.
The transducer is unloaded during the zero process.
(AngleMode=0)
Using the data collected from these two positions, all bridge zeros
and angle zeros are computed.
SWIFT 30 Sensors Setting up the Transducer Interface
63

Upload the Calibration File

Upload the Calibration File
A unique calibration file was loaded into the TI RAM by MTS before the transducer and transducer interface were shipped. Use the program TIXFER to retrieve the calibration file. TIXFER is a simple DOS-based program that will prompt you for information.
1. Connect a communication cable from the laptop computer or PC to the TI.
2. Insert the SWIFT Transducer Interface Utilities diskette into the laptop computer or PC.
3. Go to the DOS shell and run the program TIXFER.
When you type in the command to run the program, you must specify the communications port for data transfer. For example, enter TIXFER 1 to specify COM1.
4. Enter 1 at the prompt to upload the calibration file. (See the illustration below.)
5. Enter the address for the TI box at the prompt.
The address for the TI is determined by the setting of the address selector switch on the front panel. If you are using more than one transducer, each TI will have a different address.
6. Enter a file name.
The file name must use the DOS naming convention (xxxxxxxx.xxx).
7. Enter a description of the file.
You may enter the serial number of the transducer or descriptive words to help you identify the correct calibration file.
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SWIFT 30 Sensors
Upload the Calibration File
8. TIXFER will prompt you when the file has uploaded.
tixfer 1.7 beta ((10/25/04)
0...exit
1...Upload/Save a chassis
2...Restore/Download a chassis
Enter choice? 1
Enter TI box address? 1 Enter output specifications filename? demo.cal Enter description? demo upload Allocating box... Initializing box... Uploading box... Saving settings... completed upload.
SWIFT 30 Sensors Setting up the Transducer Interface
65

Edit the Calibration File

CAUTION
Edit the Calibration File
Do not change any other items in the calibration file.
The calibration file contains offset values for all of the bridge outputs. Changing any of the items other than those listed in the following procedure will cause your calibration file to be incorrect.
Take care not to change any values except those listed in the following procedure. If your calibration file is incorrectly changed, reload the original file from the diskette provided by MTS.
1. Open the calibration file using a text editor.
Setting up the Transducer Interface
66
SWIFT 30 Sensors
Edit the Calibration File
2. If necessary, edit the value for OutputPolarities.
This value sets the polarity states of all six outputs (Mz, My, Mx, Fz, Fy, and Fx) using the following binary scheme (the default configuration is represented):
O
UTPUTS MZ MY MX FZ FY FX
5
4
BIT
2
2
3222120
2
BIT VALUE
EXAMPLE
32 16 8 4 2 1
101000
= 4010 (default)
For example, if you want to invert Fx and Fy, and Mx and My, (making their polarities opposite those shown on the labeling) you would make the following changes:
M
Z MY MX FZ FY FX
5
BIT
BIT VALUE
2
32 16 8 4 2 1
4
2
2322212
10 1000= 40
11 0011
* See the examples in the next table.
0
(old value)
10
= 5110 (new value)
*
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67
Edit the Calibration File
S20-34
Front
Fz UpFyOut
Fx
Aft
Fz Up
Fx
Fore
Fy
Out
S20-35
Front
Fy
In
Fz Up
Fx
Aft
Fy
In
Fx
Fore
Fz Up
S20-41
Front
Fx Aft
Fy
In
Fz Up
Fx Aft
Fy
Out
Fz Up
Output Polarity Value
Example Output Polarities
Description
Direction of Positive output from load on tire when mounted on left hand side of the vehicle
Direction of Positive output from load on tire when mounted on right hand side of the vehicle
OutputPolarities = 40 Standard Setting from
MTS. Matches the axis orientation on the front cover of the SWIFT.
OutputPolarities = 51 Common setting to
alter the axis for-aft and in-out lateral axis
OutputPolarities (left side) = 51
OutputPolarities (right side) = 40
Common setting for vehicle coordinate matching between the two sides of the vehicle.
+Fx = fore
+Fy = out from car, left
+Fz = up
+Mx, +My+, +Mz = Right-hand rule about Force axis
+Fx = aft
+Fy= into car, right
+Fz = up
+Mx, +My, +Mz = Right-hand rule about Force axis
+Fx = aft
+Fy= into car, right
+Fz = up
+Mx, +My, +Mz = Right-hand rule about Force axis
+Fx = aft
+Fy = out from car, right
+Fz = up
+Mx, +My, +Mz = Right­hand rule about Force axis
+Fx = fore
+Fy = into car, left
+Fz = up
+Mx, +My, +Mz = Right­hand rule about Force axis
+Fx = aft
+Fy = out from car, right
+Fz = up
+Mx, +My, +Mz = Right­hand rule about Force axis
3. Perform this step for spinning application. For non-spinning applications, skip to Step 4.
A. Edit the value for ZeroAlgorithm.
The zero algorithm value that you specify will affect the operation of the Angle Zero and Bridge Zero switches.
Set ZeroAlgorithm=1, 3 or 4
1
B. Edit the value for AngleMode.
Set the AngleMode=0
In this mode, the encoder pulses are summed in with the offset and the resulting value addresses the sine and cosine RAM, which perform the rotational transformation of the output signals.
1. See the Zero Algorithms discussion on page 62 to help determine which algorithm to use.
68
Setting up the Transducer Interface
SWIFT 30 Sensors
Edit the Calibration File
C. The AngleOffset value is used when you are operating in encoder
mode (spinning applications). This value is summed with the encoder output count, and used to address the sine and cosine RAM when the angle mode is set to 0 (encoder). Negative angles are converted to their positive equivalent so that the readback value range is 0–360°.
The AngleOffset value is calculated by the TI during the zero process. At the end of the process it is written to the calibration file.
There is no need to change this calculated value.
D. Edit the value for EncoderSize depending on the SWIFT Sensor being
used.
EncoderSize=0 (sensor with telemetry option–this option is not available with the SWIFT 30 model)
EncoderSize=1 (sensor with slip ring option)
4. Perform this step for non-spinning applications. For spinning applications, skip to Step 5.
A. Edit the value for ZeroAlgorithm.
The zero algorithm value that you specify will affect the operation of the Angle Zero and Bridge Zero switches.
Set ZeroAlgorithm=0
B. Edit the value for AngleMode.
Set the AngleMode=1
In this mode, the sine and cosine RAM address is fixed. The encoder is not used, nor is the encoder offset.
C. Edit the value for AngleFixed.
The AngleFixed value is used for non-spinning applications. This value addresses the sine and cosine RAM when the angle mode is set to 1 (fixed). Negative angles are converted to their positive equivalent so that the readback value range is 0–360°.
You may set the fixed angle value when you are operating in fixed angle mode (non-spinning applications) only if the transducer is rotated from its correct Fz–Fx orientation on the road simulator. For installations where the Fz-Fx orientation on the SWIFT cover(s) is aligned with gravity. The correct setting is:
AngleFixed=0
If the SWIFT is installed at an angle to the desired Fz–Fx output axis, set the AngleFixed value equal to the installed angle offset in degrees, with clockwise rotation positive.
For example: AngleFixed = 45.
5. Save the changes and exit the editor.
SWIFT 30 Sensors Setting up the Transducer Interface
69

Download the Calibration File

Download the Calibration File
Use the program TIXFER to download the modified calibration file to the TI.
1. Insert the diskette into the laptop computer or PC.
2. Go to a DOS shell and run the program TIXFER.
When you type in the command to run the program, you must specify the communications port for data transfer. For example, enter TIXFER 1 to specify COM1.
3. Enter 2 at the prompt to download the calibration file.
4. Enter the address for the TI box at the prompt.
The address for the TI is determined by the setting of the address selector switch on the front panel. If you are using more than one transducer, each TI will have a different address.
5. Enter the name of the file you wish to download.
The file must be in the same directory as the TIXFER program. The file name must use the DOS naming convention (xxxxxxxx.xxx), which means that you must type the full name and the extension.
6. TIXFER will prompt you when the file has successfully downloaded.
Setting up the Transducer Interface
70
SWIFT 30 Sensors
7. Enter 0 at the prompt to exit the program.
tixfer 1.7 beta ((10/25/04)
0...exit
1...Upload/Save a chassis
2...Restore/Download a chassis
Enter choice? 2
Enter TI box address? 1 Enter input specifications filename? demo.cal Allocating box... Initializing box... Restoring settings... Downloading box... Completed download.
tixfer 1.7 beta ((10/25/04)
Download the Calibration File
0...exit
1...Upload/Save a chassis
2...Restore/Download a chassis
Enter choice? 0 Program completed
SWIFT 30 Sensors Setting up the Transducer Interface
71
Download the Calibration File
Setting up the Transducer Interface
72
SWIFT 30 Sensors

Installing the Transducer

The SWIFT sensor can be installed on a vehicle at the test track or on an MTS Series 329 Road Simulator in the test laboratory.
Contents Test Track Vehicle 74
Attaching SWIFT Components to the Vehicle 78
Installing the Transducer Interface Electronics 83
Setting up the SWIFT Sensor for Data Collection 85
Verifying the Quality of the Zero Procedure 95
Collecting Data 97
Road Simulator 99
Attaching SWIFT Components to the Fixturing 101
Zeroing the Transducer Interface 104
Communication Configurations 105
Cable Configurations 106
SWIFT 30 Sensors Installing the Transducer
73

Test Track Vehicle

Test Track Vehicle
Equipment required This procedure requires one person. To install the SWIFT 30A or SWIFT 30T
sensor, you will need the following equipment:
Hub adapter (see next figure)
Modified rim (see next figure)
Anti-rotate assembly (including customer-supplied mounting arm)
Small set of hex-head wrenches (both English and metric)
Tube bender for the anti-rotate bar
Tube cutter
Metric socket head drive set (up to 14 mm) with extension
5/16-18 UNC tap
Molykote g-n paste (MTS part number 011-010-207)
Bolts
For SWIFT 30A Transducer
48 size M10 X 1.5 mm
4 size M8 X 1.25 mm
8 size M5 X 0.8 mm
lug nuts
For SWIFT 30T Transducer
48 size M10 X 1.5 mm
4 size M8 X 1.25 mm
8 size M5 X 0.8 mm
Lug nuts
Torque wrenches, capable of the following ranges:
28–54 N•m (20–40 lbf•ft),
81–136 N•m (60-100 lbf•ft);
7 N•m (60 lbf •in)
Installing the Transducer
74
Cables (transducer and BNC, plus customer-supplied from transducer
interface to data recorder)
Tie wraps
Data recorder
12 V power supply (for example, a car battery)
SWIFT 30 Sensors
Test Track Vehicle
S20-03
Transducer
Hub Adapter
Slip Ring
(with Encoder)
Modified
Wheel Rim
Slip Ring
Bracket
(Spider)
CAUTION
Installation Components (Test Track)
Importance of bolts Bolts provide exceptional clamp force at the transducer to rim/spindle interface.
Bolts on the inner hub secure the hub adapter to the SWIFT sensor.
Before you begin Observe the following safety conditions while you are attaching the SWIFT
Bolts on the outer ring secure the SWIFT sensor to the wheel rim (or road
simulator spindle adapter).
Note Make sure all bolts are in place and fully torqued during all tests.
Correct use of bolts reduces the safety hazard and ensures optimal transducer performance.
sensor and components to the vehicle.
Do not pressure-wash the transducer or clean it with solvents that would degrade its silastic seal.
Pressure-washing the transducer or cleaning it with certain solvents can damage it or degrade its silastic seal.
Avoid pressure-washing the transducer. Use only solvents that will not degrade the silastic seal.
SWIFT 30 Sensors Installing the Transducer
75
Test Track Vehicle
CAUTION
CAUTION
CAUTION
CAUTION
Do not use high-pressure-air to clean debris from around the transducer connectors.
High-pressure-air can damage the silastic seals.
Use a fine wire brush and low air-pressure [0.07 MPa (10 psi)] to clean debris from around the transducer connectors.
Do not lay the wheel flat while the transducer is attached to it.
When the wheel is laid flat with the transducer facing down the weight of the wheel can damage the connectors.
Always hold the wheel upright when the transducer is attached to it. If needed, have another person hold the tire upright while you tighten the bolts, or place the wheel on a thin layer of foam to protect the connectors.
Do not under-torque the lug nuts.
Lug nuts that are not properly tightened can become loose during testing. Loss of a wheel can cause damage to the test vehicle and transducer and result in injury to personnel.
Always tighten the lug nuts to the torque rating recommended for the vehicle/ wheel.
Do not drop the slip ring bracket (spider).
Dropping the slip ring bracket can damage the slip ring or a connector.
Always use care when you handle the slip ring bracket.
Installing the Transducer
76
SWIFT 30 Sensors
Test Track Vehicle
CAUTION
Do not allow the mounting arm or anti-rotate arm to bump against any portion of the wheel or wheel well.
The anti-rotate device should not bump against the wheel well or other vehicle parts at any time. Any jarring of the anti-rotate arm will damage the slip ring and/or the encoder.
Position the mounting arm and anti-rotate assembly so that full suspension travel will not cause interference with the wheel well or any other part of the vehicle.
SWIFT 30 Sensors Installing the Transducer
77
Test Track Vehicle

Attaching SWIFT Components to the Vehicle

SWIFT 30 Fasteners
M10 X 1.5 mm
M8 X 1.25 mm
M5 X 0.8 mm
MTS modified M12 X 1.5 mm
or 1/2–20UNF inch lug nuts
* For threaded spindle applications, customer
supplied M12 or 1/2 in fasteners of appropriate length and thread pitch are required.
*
Procedure 1. Remove the current wheel from the test vehicle.
2. Clean all surfaces of the vehicle tire(s) and the modified rim(s). It is critical that all surfaces be free of stones, burrs, and grease. Use a mild detergent such as dish soap.
Important It is imperative that the mounting surfaces of the transducer be
protected from getting scratched. Any wheel components and work surfaces that might come in contact with the transducer must be clean, smooth, and free of debris
Mount the tire(s) on the modified rim(s).
3. Wipe the unpainted mating surfaces of the modified rim and the transducer with a clean dry cloth.
4. Attach the transducer to the modified wheel rim. Hand tighten the bolts.
If environmental conditions warrant, coat each fastener with Birchwood Casey Sheath RB1 rust preventative (or equivalent).
Installing the Transducer
78
Lubricate the threads and under the heads of all fasteners, using Molykote g-n paste.
SWIFT 30 Sensors
Test Track Vehicle
SWIFT 30A or SWIFT 30T
Viewed from Pilot Side
S30-16
Inner Bolt Pattern
Bolts AD are M8
Bolts 124 are M10
Outer Bolt Pattern
All bolts are M10
B
A
8
4
16
11
19
23
14
2
D
6
10
18
22
15
3
7
12
20
24
13
21
17
9
5
C
1
4
16
21
17
9
5
1
13
24
20
12
7
3
15
22
18
10
6
2
14
23
19
11
8
5. Attach the hub adapter to the transducer. Hand tighten the bolts.
If environmental conditions warrant, coat each fastener with Birchwood Casey Sheath RB1 rust preventative (or equivalent).
Lubricate the threads and under the heads of all fasteners, using Molykote g-n paste.
A clearance of approximately 0.05 mm (0.002 in) is required between the transducer and the hub adapter. You should not have to wedge the wheel into the rim or the hub adapter into the SWIFT sensor.
Bolt Torque Sequence
6. Tighten the mounting bolts.
A. Following the sequence shown in the previous figure for the transducer
Important The M8 bolts in the inner bolt pattern (bolts A–D in the previous
being installed, torque the four M8 inner hub bolts in two increments as shown in the following table.
figure) must be torqued, as described, before torquing the M10 bolts.
B. Following the sequence shown in the previous figure for the transducer
being installed, torque the twenty-four M10 inner hub bolts in two increments as shown in the following table.
SWIFT 30 Sensors Installing the Transducer
79
Test Track Vehicle
Note To minimize negative clamping effects, you must torque the bolts in the
sequence shown.
B
OLT SIZE
TORQUE INCREMENT M8 M10
1st Increment
Final Torque
14 N•m (10 lbf•ft) 27 N•m (20 lbf•ft)
27 N•m (20 lbf•ft) 54 N•m (40 lbf•ft)
C. Following the sequence shown in the previous figure for the transducer
being installed, torque the twenty-four M10 outer hub bolts in two increments as shown in the previous table. See the previous note.
Installing the Transducer
80
SWIFT 30 Sensors

Attaching SWIFT and Wheel Assembly to the Vehicle

1. Before installing the SWIFT and wheel assembly, attach the slip ring anti­rotate bracket to the vehicle.
Since the bracket is unique to each vehicle the slip ring anti-rotate bracket must be provided by the customer. The following are guidelines for manufacturing and locating the bracket. See the next figure.
The bracket must be stiff, preferably steel or stiff aluminum tubing, so
as not to move or rotate when connected to an unsprung mass or spindle which will allow the slip ring assembly to move with the tire as the vehicle is moving or testing.
The bracket must be positioned so as not to hit the fender at the
extreme end of the suspension travel.
The bracket must maintain a minimum clearance from the tire so as not
to hit the tire when it is loaded and rotating.
2. Attach the wheel/transducer to the test vehicle.
Test Track Vehicle
Lubricate the lug bolt threads with Molykote g-n paste.
Tighten the lug nuts to the torque rating recommended for the wheel.
3. Attach the slip ring bracket (spider) and slip ring to the transducer.
A. The slip-ring bracket fits over the 10-pin connectors on the front of the
transducer at the locations labeled Board A and Board B. The slip-ring bracket is similarly labeled to prevent connecting it the wrong way.
Note Use care when installing the slip-ring bracket. The 10-pin connectors are
keyed. The slip-ring bracket should be fitted on straight (without bending or angling it) to make sure it engages both connectors simultaneously and evenly.
B. Lubricate the threads and under the bolt heads of the eight M5 X 0.8
mm bolts with Molykote g-n paste. Insert them through the mounting hole in the slip ring bracket and thread them into the transducer. Torque them to 6.8 N•m (60 lbf•in).
C. Make sure that the covers on the shunt connectors are securely locked
in place. Each cover should be twisted until it snaps into the retaining groove.
4. Attach the anti-rotate assembly to the anti-rotate bracket (installed earlier) and the slip ring. If this is the first time the anti-rotate assembly is used on this vehicle or if the mounting location has changed, perform Steps A and B, otherwise proceed to Step C. (Refer to the next figure for guidelines.)
A. Weld the steel tube sleeve to the customer-supplied customer supplied
anti-rotate bracket.
B. Bend the aluminum tube to fit over the wheel.
SWIFT 30 Sensors Installing the Transducer
81
Test Track Vehicle
Slip Ring
Assembly
Suspension/
Unsprung Mass
Minimum Clearance
Typically approximately
6 mm (0.25 in) depending
on tire uniformity. Tire
must not hit bracket when
loaded or rotating.
Anti-Rotate Bracket
must be Stiff (preferably steel
or stiff aluminum tubing), so as
not to move or rotate when
connected to unsprung mass
or spindle, which will allow the
slip ring assembly to move with
the tire as the vehicle is
moving or testing.
Center line
of Wheel
Anti-Rotate
Assembly
Transducer
5/16-18 UNC
Low-head Socket Screw
19 mm (0.75 in) long
Steel
Sleeve
Modified Delrin Ball
15.875 mm (0.625 in) diameter
Vehicle Fender
Bracket must not hit
fender at extreme end
of suspension travel
Weld steel sleeve to
anti-rotate bracket
when assembly is
mounted on vehicle
S30-18
M4 X 0.7 mm X10 mm long
or 8-32 X 3/8 in long
Socket Head
Cap Screw (qty 2)
Transducer
Output Cable
C. Measure, making bends as necessary, and cut the aluminum tube to
size.
MTS provides an extra long tube with a hinge welded at one end. After fitting the tube to your test vehicle, cut off the excess length.
D. Tap the end of the aluminum tube 5/16-18 UNC X 1.00 inch deep.
E. Insert the low-head cap screw through the delrin ball.
F. Insert the aluminum tube into the steel sleeve.
G. Tighten the screws that attach the hinge joint to the slip ring assembly.
82
Installing the Transducer
5. Attach the transducer output cable to the slip ring encoder connector and the Slip Ring D-connector on the rear of the TI.
6. Secure the cable along its length so that ot will not become damaged during data collection. (For example, tape it to the external mirror.)
Be sure to leave enough slack in the cable to allow for the full range of wheel travel (jounce and steer).
SWIFT 30 Sensors

Installing the Transducer Interface Electronics

The Transducer Interface (TI) electronics should be securely fastened to the vehicle in a protected location. The TI box is designed to withstand the accelerations associated with the body of a vehicle during rugged durability and typical data acquisition testing.
The TI box can be located anywhere in the vehicle that is convenient. However, if the TI is able to bounce around during data collection, it can bump against another piece of equipment, pushing in the Zero button. If the Zero button is pushed, you will lose all of the data.
Considerations Suitable locations for the TI box include the vehicle trunk, flatbed, interior floor,
or rear seat. Consider the following guidelines when you fasten the TI box(es) to the vehicle:
Mount the TI box in a position on or in the vehicle that is protected from
impact and high acceleration events.
Do not expose the TI box to rain, snow, or other wet conditions.
Test Track Vehicle
Orient the TI box horizontally.
Multiple TI boxes may be rigidly attached to each other using optional
mounting straps.
Place a thin foam or rubber material between TI boxes and any hard
mounting surface.
Use ratcheting straps to provide a tight connection that will not loosen or
untie during testing.
Do not use rubber cords to secure the TI box because they may stretch and
lose retention in the cord due to inertial forces.
Procedure 1. Connect all data cables from the TI to the data recorder.
There is one cable per channel of data from the TI to the data recorder. These correspond to the three forces, three moments, and angular position.
Note Make sure that there is no tension or strain in the cables or at the cable
and connector junction. There should be some slack in the cables to ensure that they are not pulled during testing.
2. Connect the TI and the data recorder to a 12 V DC power source (such as a vehicle battery).
Note Some data acquisition systems may introduce electrical noise spikes to
the battery and cabling. The TI electronics should always be used with the cleanest power supply possible. To reduce the likelihood of noise spikes from the data recorder, we suggest running the power cables in parallel, as shown in the following diagrams. If this does not remove the noise spikes, separate batteries may be required.
SWIFT 30 Sensors Installing the Transducer
83
Test Track Vehicle
Ground to vehicle frame
12 Vdc
Transducer Interface
S50-025
Data Recorder
Ground to vehicle frame
12 Vdc
Transducer Interface
Transducer Interface
Transducer Interface
Transducer Interface
S50-026
Data Recorder
3. Ground the TI and data recorder to the vehicle frame. (See the following figures.)
Suggested Grounding for a single TI Box
Installing the Transducer
84
Suggested Grounding for a Multiple TI Boxes
4. Secure the TI box so that it will not move during data collection.
Note If the TI box is not properly secured, it can bump against another piece of
equipment or a hard surface, pushing in the Zero button. If the Zero button is pushed, you will lose all of the data.
5. Verify that the shunt contacts are covered.
Make sure that the plugs on the slip ring bracket (spider) cover are in place so that no water will enter the contacts.
Make sure that the bayonette covers on the shunt connectors are securely locked in place. Each cover should be twisted until it snaps into the retaining groove.
6. Turn on the TI and let it warm up for 15-20 minutes before you zero the
SWIFT 30 Sensors
strain gage bridges.

Setting up the SWIFT Sensor for Data Collection

CAUTION
CAUTION
To ensure accurate data collection, complete this setup procedure daily before you begin testing.
The accuracy of the data that you collect depends on the ability of the SWIFT electronics to “zero out” the forces and angles present in an initial, unloaded state. During the Zero process, the TI box reads the transducer bridge values and compensates for any offsets so that the bridge output is 0 at 0.0 V. It also reads the current angle and compensates for any offset from the Z axis facing up.
You can ensure the success of the Zero procedure by taking these simple precautions:
Do not introduce extraneous forces or excessive accelerations into the wheel while rotating it during the Zero process.
Test Track Vehicle
Considerations for
rotating a tire
Any forces applied to the wheel, tire, rim, spider, or outer portion of the transducer will cause a Bridge Zero error.
Make sure to apply only a gentle force at a steady rate to the inner hub while rotating it.
Do not touch or bump the wheel while the transducer is zeroing.
Touching or bumping the wheel will add loads to the transducer, resulting in an erroneous zero reading.
Avoid all contact with the wheel while the transducer is zeroing. If you suspect that the zero process is incorrect, begin again
When using a zero method that collects zero data while the sensor is rotating (i.e., algorithm 1 or 3), you must be careful to minimize the forces that are induced in the transducer’s bridges.
When using one of these zero methods, never rotate the tire directly, or by grabbing the outer diameter of the transducer. This will introduce forces into the transducer bridges that will result in a bad zero process and unreliable data.
Rotate the tire at an even rate to avoid accelerations on the transducer.
For positive-lock differentials, turn the other tire on the axle to cause the
desired rotation in the transducer you are zeroing.
If you must touch the transducer to rotate the tire, carefully rotate the tire by
touching only the inner diameter of the transducer.
SWIFT 30 Sensors Installing the Transducer
85
Test Track Vehicle
Choosing a Zero
method
Preferred method—Zero Algorithm 4 is the preferred method for configuring the calibration file for spinning applications:
ZeroAlgorithm=4
AngleMode=0
This zero method samples all eight input bridges at two positions. After the data is taken, all eight input channels are analyzed for signal offsets, and bridge zeroes and angle zeroes are set in the TI.
Alternate methods—Zero Algorithm 1 and 3 are alternate methods for configuring the calibration file:
ZeroAlgorithm=1
AngleMode=0
Zero Algorithm 1 samples all eight input bridges on every encoder tick, for one complete revolution. After the data is taken, all eight input channels are analyzed for signal offsets, and bridge zeroes are set in the TI. The angle offset is then recorded in a separate step.
ZeroAlgorithm=3
AngleMode=0
Zero Algorithm 3 may be more convenient for some test setups. However, you must take care when using it, because it is susceptible to two types of errors:
Noise spikes from power. These can be minimized by following the
grounding suggestions illustrated earlier in this chapter.
Extraneous loads. Be very careful to rotate the wheel only by touching the
inner hub of the transducer or by engaging the axle (for some vehicles, this means putting the vehicle in Park) and rotating the opposite wheel.
Because the SWIFT sensor measures loads applied to the outer edge of the transducer, you should never touch the outer edge while you are spinning the wheel. The rotation speed should be smooth, in order to avoid applying inertial braking moments to the transducer.
Installing the Transducer
86
SWIFT 30 Sensors
Test Track Vehicle
[SWIFT] Name=zero 3 after new tire SerialNum=1234567 Normalization=0 InputSwitches=255 OutputPolarities=40 ZeroAlgorithm=4 AngleMode=0 AngleOffset=82.0898 AngleFixed=0 EncoderSize=1 ZFX1=0.103786 ZFX2=-0.023199 ZFY1=-0.094017 ZFY2=-0.184371 ZFY3=-0.225885 ZFY4=-0.269841 ZFZ1=-0.101343 ZFZ2=-0.045177 KFX1=0.196337 KFX2=0.195604 KFY1=0.169231 KFY2=0.166789 KFY3=0.167277 KFY4=0.16801 KFZ1=0.195849 KFZ2=0.196581 KMX=3.7558 KMYX=2.39805 KMYZ=2.5641 KMZ=3.75824 KFXFY=0.000611 KFXFZ=-0.00315 KFXMX=0.008864 KFXMY=-0.005348
S20-38
Zero Algorithm
0 Non-spinning mode 1 Spinning mode (uses a digital
inclinometer for angle zero and spinning the tire for the bridge zero
process 2 Not used 3 Spinning mode (uses spinning the
tire for both angle and bridge
processes) 4 Spinning mode (use a digital
inclinometer to define two positions
90° apart for the bridge zero and
angle zero processes.
Angle Mode
0 Spinning mode (obtains angle from
the encoder) 1 Fixed angle mode (used for test rigs
in the lab)
This zero method samples all eight input bridges on every encoder tick, for one complete revolution. After the data is taken, all eight input channels are analyzed for signal offsets, and the X and Z input channels are analyzed to determine the angular zero point.
SWIFT 30 Sensors Installing the Transducer
Example of a .cal file
If Zero Algorithm=4 When you zero the TI, you want the vehicle to be fairly level and the transducer
to be as close to plumb as practical.
1. Install the SWIFT sensor(s) and data collection equipment on the vehicle.
2. Connect all cables and turn on the power to the TI boxes.
3. Let the TI boxes and transducers warm up for 15-20 minutes.
4. Run the TISTATUS program to compare the supply voltages to the
5. Verify that the calibration file is set up correctly for your testing application.
reference voltages.
Type: TIstatus <port#> <box#>
If the supply voltages vary more than 0.5 V from the reference voltages, there is a power supply problem that must be resolved before you can continue.
87
Test Track Vehicle
Axes Icon
S20-22
A. Download the spinning calibration file (xxxxxs.cal) to the computer
from the MTS Disk that corresponds to the serial number of the transducer that you are setting up.
B. If necessary, modify the zero algorithm and angle mode to fit the
application/use requirements as described in, “Edit the Calibration
File,” on page 66.
C. The EncoderSize parameter should be omitted or set to EncoderSize=1
D. Download the calibration file to the TI box.
Note If it becomes necessary to change the zero algorithm or angle mode
after downloading the file to the TI, you can do so by using the TISETZERO utility, as described in, “TISETZERO – Transducer Interface
Set Zero Method,” on page 55.
6. Elevate the vehicle with a lift, raise each corner with a jack.
7. Perform the zero procedure on each corner of the vehicle.
Use a digital inclinometer to zero the angle and strain gage bridges on the transducer.
A. Rotate the tire one full revolution so that the encoder can find the zero
index mark.
Note The encoder has a red dot on the mounting flange connected to the slip-
ring bracket and a black dot on the slip-ring connector housing where it interfaces with the mounting flange. These dots, when aligned next to each other, indicate the index mark is under the encoder sensor.
B. Rotate the tire as necessary, until the Fz on the axes icon (see the next
figure) printed on the transducer label is pointing up
C. Attach the level bracket so that it sits on top of the transducer. Insert the
locking pin through the bracket and into the pin pilot hole on the transducer (see the next figure).
Installing the Transducer
88
SWIFT 30 Sensors
Test Track Vehicle
Digital Inclinometer
in this position
should read 0°, ±0.1°
Axes Icon
Insert Lock Pin
in Pilot Hole
Level Bracket
S30-20
Digital Inclinometer
(alternate location)
in this position
should read 90°, ±0.1°
S20-21
Angle Zero
Switch and Indicator
Bridge Zero
Switch and Indicator
Note If the anti-rotate assembly interferes with the mounting of the digital
inclinometer, use the alternate mounting location shown.
D. Place the digital inclinometer on the bracket and rotate the tire until the
inclinometer reads 0.0°, ±0.1° (or 90.0°, ±0.1° if the alternate position is used).
E. Push the Bridge Zero button on the front of the TI box. The LED will
turn on for a few seconds, then start blinking rapidly. The Angle Zero indicator will start blinking slowly.
F. Remove the digital inclinometer and level bracket.
G. Rotate the tire 90° in either direction.
H. Attach the level bracket in the same orientation as in Step 7C.
Insert the locking pin through the bracket and into the pin pilot hole on the transducer.
SWIFT 30 Sensors Installing the Transducer
89
Test Track Vehicle
Digital Inclinometer
in this position
should read 0°, ±0.1°
Insert Lock Pin
in Pilot Hole
Level Bracket
S30-23
Rotate Transducer
+ or - 90°
Digital Inclinometer
(alternate location)
in this position
should read 90°, ±0.1°
I. Place the digital inclinometer on the bracket and rotate the tire until the
inclinometer reads 0.0°, ±0.1° (or 90.0°, ±0.1° if the alternate position is used).
J. Push the Angle Zero button on the front of the TI box. The Angle Zero
indicator will light for a few seconds, then both the Bridge Zero and Angle Zero indicators should turn off.
Note If the red Fail indicator lights momentarily and the Bridge Zero and
Angle Zero indicators end up blinking slowly, problems were detected
with the zero. Try repeating the procedure. Use TISTATUS for a more detailed explanation of the problem. If you continue to have an error, consult the chapter, “Troubleshooting,” on page 127.
K. Rotate the transducer slightly to update the rotational transformation.
At this point the TI should be reading absolute forces in the vehicle coordinate system.
L. Perform, “Verifying the Quality of the Zero Procedure,” on page 95.
M. Look at your data acquisition system to verify that the SWIFT sensor is
If Zero Algorithm=1 When you zero the TI, you want the vehicle to be fairly level and the transducer
to be as close to plumb as practical.
1. Install the SWIFT sensor(s) and data collection equipment on the vehicle.
2. Connect all cables and turn on the power to the TI boxes.
gathering data.
3. Let the TI boxes and transducers warm up for 15-20 minutes.
Installing the Transducer
90
SWIFT 30 Sensors
Test Track Vehicle
4. Run the TISTATUS program to compare the supply voltages to the reference voltages.
Type: TIstatus <port#> <box#>
If the supply voltages vary more than 0.5 V from the reference voltages, there is a power supply problem that must be resolved before you can continue.
5. Verify that the calibration file is set up correctly for your testing application.
A. Download the spinning calibration file (xxxxxs.cal) to the computer
from the MTS Disk that corresponds to the serial number of the transducer that you are setting up.
B. If necessary, modify the zero algorithm and angle mode to fit the
application/use requirements as described in, “Edit the Calibration
File,” on page 66.
C. The EncoderSize parameter should be omitted or set to EncoderSize=1
D. Download the calibration file to the TI box.
Note If it becomes necessary to change the zero algorithm or angle mode
after downloading the file to the TI, you can do so by using the TISETZERO utility, as described in, “TISETZERO – Transducer Interface
Set Zero Method,” on page 55.
6. Put the vehicle on a lift or jack up the corner of the vehicle on which the SWIFT sensor is mounted.
Important Place wheel chocks under the wheels on the ground or otherwise
restrain the vehicle to prevent it from moving.
7. Push the Bridge Zero button. Only the Bridge Zero indicator will light.
8. Gently spin by hand, the wheel on the opposite side of the vehicle for two revolutions. Be careful not to allow the wheel to stop or reverse direction.
This will cause the wheel you are zeroing to spin without load.
Note For rear wheels or wheels where this cannot be done, carefully spin the
wheel to be zeroed by gently contacting only the hub adapter bolted to the SWIFT sensor.
9. Stop spinning the wheel when the Bridge Zero indicator begins to blink at a rate of 4 Hz and continues blinking for about one minute.
The Bridge Zero indicator will then turn off, indicating completion of the Bridge Zero procedure.
10. Perform the Angle Zero procedure.
Use a digital inclinometer to zero the angle on the transducer, then rotate the tire to zero the strain gage bridges.
A. Rotate the tire one full revolution so that the encoder will pass the zero
index mark at least once.
SWIFT 30 Sensors Installing the Transducer
91
Test Track Vehicle
Axes Icon
S20-22
Digital Inclinometer
in this position
should read 0°, ±0.1°
Axes Icon
Insert Lock Pin
in Pilot Hole
Level Bracket
S30-20
Digital Inclinometer
(alternate location)
in this position
should read 90°, ±0.1°
Note The encoder has a red dot on the mounting flange connected to the slip-
ring bracket and a black dot on the slip-ring connector housing where it interfaces with the mounting flange. These dots, when aligned next to each other, indicate the index mark is under the encoder sensor.
B. Rotate the tire as necessary, until the Fz on the axes icon (see the next
figure) printed on the transducer label is pointing up
C. Attach the level bracket so that it sits on top of the transducer. Insert the
locking pin through the bracket and into the pin pilot hole on the transducer (see the next figure).
Note If the anti-rotate assembly interferes with the mounting of the digital
inclinometer, use the alternate mounting location shown.
Installing the Transducer
92
D. Place the digital inclinometer on the bracket and rotate the tire until the
inclinometer reads 0.0°, ±0.1° (or 90.0°, ±0.1° if the alternate position is used).
E. Push the Angle Zero button on the front of the TI box. The Angle Zero
indicator will turn on for a few seconds, then turn off indicating that the Angle Zero procedure is complete.
11. After completing the Bridge and Angle Zero procedures, rotate the wheel one full revolution clockwise.
This allows the electronics to locate the index pulse for the encoder.
SWIFT 30 Sensors
Test Track Vehicle
Note The wheel must rotate one-half revolution in the same direction and then
pass over the encoder index point before data collection is started.
12. Perform, “Verifying the Quality of the Zero Procedure,” on page 95.
13. Look at your data acquisition system to verify that the SWIFT sensor is gathering data.
If Zero Algorithm=3 When you zero the TI, you want the vehicle to be fairly level and the transducer
to be as close to plumb as practical.
1. Install the SWIFT sensor(s) and data collection equipment on the vehicle.
2. Connect all cables and turn on the power to the TI boxes.
3. Let the TI boxes and transducers warm up for 15–20 minutes.
4. Run the TISTATUS program to compare the supply voltages to the reference voltages.
Type: TIstatus <port#> <box#>
If the supply voltages vary more than 0.5 V from the reference voltages, there is a power supply problem that must be resolved before you can continue.
5. Verify that the calibration file is set up correctly.
A. Download the calibration file (xxxxx.cal) to the computer from the
MTS Disk that corresponds to the serial number of the transducer that you are setting up.
B. If necessary, modify the zero algorithm and angle mode to fit the
application/use requirements as described in, “Edit the Calibration
File,” on page 66.
C. The EncoderSize parameter should be omitted or set to EncoderSize=1
D. Download the calibration file to the TI box.
Note If it becomes necessary to change the zero algorithm or angle mode
after downloading the file to the TI, you can do so by using the TISETZERO utility, as described in, “TISETZERO – Transducer Interface
Set Zero Method,” on page 55.
6. Elevate the vehicle with a lift, or raise each corner with a jack.
7. Perform the zero procedure on each corner of the vehicle. Both the angle and bridge zeros are computed by rotating the tire.
SWIFT 30 Sensors Installing the Transducer
93
Test Track Vehicle
S20-21
Angle Zero
Switch and Indicator
Bridge Zero
Switch and Indicator
A. Push either the Angle Zero or Bridge Zero button on the front of the
TI box. Both indicators will light.
B. Rotate the tire 1 1/4 to 2 revolutions, until the Bridge Zero indicator
starts flashing. Follow the guidelines in, “Considerations for rotating a
tire,” on page 85.
C. If the Bridge Zero indicator continues to slowly flash after 2 minutes,
or if the red Fail indicator flashes, there is an error in the zero process. Run TISTATUS to find out more information. Repeat Steps A and B. If you continue to have an error, consult the chapter, “Troubleshooting,” on page 127.
D. Perform, “Verifying the Quality of the Zero Procedure,” on page 95.
E. Look at your data acquisition system to verify that the SWIFT sensor is
gathering data.
Installing the Transducer
94
SWIFT 30 Sensors

Verifying the Quality of the Zero Procedure

Connect to
Data Acquisition
System
Shunt A
Board A
Board A
Shunt B
S30-24
Perform the following consistency checks for each SWIFT sensor while the vehicle (or corner) is elevated.
1. Does Fz measure the approximate weight of the tire/rim assembly?
2. Is Fx small (less than 0.1% of the rated load)?
3. What is the variance in Fz (modulation) when the tire is slowly rotated?
4. When the vehicle is on the ground, is the Fz reading approximately equal to the corner weight of the vehicle? (See, “Effect of Zero Reference on SWIFT
Output,” on page 96.)
Acceptable Variations for Fx, Fz Readings
T
RANSDUCER MODEL MAX RATED LOAD
(F
X, FZ)
X READING
F
WITH VEHICLE LIFTED
Test Track Vehicle
FZ MODULATION
WITH VEHICLE LIFTED
SWIFT 30 A (Aluminum)
SWIFT 30T (Titanium)
28 kN 0.1% (±20–30 N) 0.2% (±40–60 N)
50 kN 0.1% (±40–50 N) 0.2% (±60–100 N)
5. Perform a Shunt calibration on each transducer.
A. Elevate the vehicle on a lift, or jack up each corner.
B. Connect the shunt calibration cables from the Shunt A, Shunt B
connectors on the front of the transducer to the Shunt A, Shunt B connectors on the back of the TI box (see the next figure).
C. Connect the signal cable from the slip ring to the Slip Ring connector
on the back of the TI box.
D. Press the Shunt button on the front of the TI box, or use option 5 in the
TISHUNT program.
The shunt indicator will light continuously for 30–45 seconds. If the indicator continues to flash after shunt calibration is complete, the shunt calibration has failed.
Connect the shunt calibration cables
SWIFT 30 Sensors Installing the Transducer
95
Test Track Vehicle
6. Verify that the outputs from the TI box matches those on the calibration report.
Use either the TISHUNT or TIXFER program to look at the shunt values of the individual bridges.
The shunt calibration will fail if the measured shunt values are >2% of the reference values that were set at the factory. Typically, the shunt values will vary a maximum of 0.20-0.30 V from the reference values.
Refer to the chapter, “Troubleshooting,” on page 127, for more information on dealing with shunt calibration failures.
Effect of Zero
Reference on SWIFT
Output
When the SWIFT sensor is used in spinning applications, it is important that a correct absolute zero of each strain gage bridge is used to ensure the proper computation and transformation of the transducer outputs to a non-rotating vehicle coordinate system. An error in the absolute zero of each bridge will produce a one-time-per-revolution modulation error in the output signals. To achieve absolute zero of each bridge, the zeroing process must account for the tare weight acting on the transducer.
When the vehicle is lifted and the tire and wheel assembly are suspended, the mass of the tire, rim, outer diameter fasteners, and outer ring of the transducer are all reacted through the beams of the transducer. With gravity acting on this outer tire/rim assembly, the SWIFT sensor measures a vertical force pulling down on the transducer.
The SWIFT output cannot be zero, because it is not possible to set the vehicle on the ground precisely enough that the ground supports only the outer tire/rim weight.
As the vehicle is set completely on the ground, the output from the SWIFT sensor will read the corner weight of the vehicle from the reference point of the transducer. The output of the SWIFT sensor will be slightly less than the total corner weight of the vehicle, because the SWIFT sensor is inboard of the outer tire and rim assembly, and will therefore not measure the weight of the outer tire and rim assembly.
Installing the Transducer
96
SWIFT 30 Sensors

Collecting Data

Test Track Vehicle
After you zero the TI, you are ready to collect data.
Note If you turn off power to the TI boxes, the zero values will remain valid, but
the encoder will need to find the index pulse to properly convert the rotating coordinates to stationary coordinates. The transducer outputs will not be correct until this happens.
To reset the encoder, roll the vehicle either forward or backward so that the tire completes at least one revolution. This can be accomplished while driving to the test area, or if the vehicle is on a lift in the garage area, rotate the tire according to the guidelines in , “Considerations for
rotating a tire,” on page 85.
1. Spin the wheel twice to ensure that the encoder tick is correct.
Spinning the wheel after you have completed the zero process will ensure that the encoder is correctly referenced to the index pulse. Otherwise, the data collected during the first revolution will be flawed.
2. Remove the vehicle from the lift or jacks.
3. Secure the connector that attaches the signal cable to the top of the slip ring with high quality duct or electrical tape.
This will prevent dust, dirt, and water from entering the connector and causing wear on the pins and sockets.
4. Verify that the shunt contacts are covered.
Ensure that the plugs on the slip ring bracket (spider) cover are in place so that no water will enter the contacts.
Ensure that the covers on the shunt connectors are securely locked in place. Each cover should be twisted until it snaps into the retaining groove.
5. Perform a final inspection of the SWIFT sensor and the electronics to ensure that everything is secure and the TI is on.
The zero data is saved at the end of each completed procedure. If the TI is off, the zero data will not be lost. However, due to thermal conditions that could affect your data, if the TI is powered off for an extended period of time (such as over night), you must repeat the zero process.
Note Rezeroing the transducer is good practice when thermal changes occur.
Rezeroing the transducer at conditions and temperatures closest to the test conditions will provide a more accurate zero and reduce thermal errors.
6. Turn on the data recorder.
7. Start data collection.
Important Before beginning data collection, read the cautions on the next
page.
SWIFT 30 Sensors Installing the Transducer
97
Test Track Vehicle
CAUTION
CAUTION
WARNING
WARNING
Do not allow the SWIFT assembly to bump into any hard surfaces while you are driving the vehicle.
Bumping the SWIFT assembly into hard surfaces such as garage doors, ramps and railings will damage the anti-rotate device, cable, slip ring, slip ring bracket (spider), and transducer.
The SWIFT assembly will protrude approximately four inches (102 mm) from the side of the vehicle. Remember to allow extra space on each side of the test vehicle as you enter and exit areas with possible hazards.
Do not drive through tall grass and brush.
Driving through tall grass and brush can damage the cable and tear off the slip ring.
Avoid areas of the test track with tall grass and brush.
Do not use the SWIFT sensor on public roads.
Public use or use on public roads could endanger the public.
Use the SWIFT sensor only on closed courses where the loads and load cycles are recorded and managed within the prescribed limits. Only experienced test vehicle drivers should operate a vehicle with the SWIFT sensor attached
Do not use the SWIFT sensor after excessive loading or load cycles.
The SWIFT sensor has a limited load life. Excessive loading or load cycles could cause a fracture of the transducer, wheel rim, hub adapter, or fasteners and can result in injury or death.
Always be aware of the maximum full scale loads appropriate for your transducer. Upon approaching a prescribed limit, return the transducer with the recorded load cycles to MTS for physical inspection and analysis of the load cycle history
Installing the Transducer
98
SWIFT 30 Sensors

Road Simulator

CAUTION
CAUTION
CAUTION
Before you begin Angular correction is required on the test track only. If you are using the same
transducer(s) for non-spinning simulation testing you must load the correct software into the TI.
The SWIFT sensor must be attached to the test fixture before the vehicle is mounted.
Clean all surfaces. It is critical that all surfaces be free of stones, burrs, and grease.
Do not pressure-wash the transducer or clean it with solvents that would degrade its silastic seal.
Pressure-washing the transducer or cleaning it with certain solvents can damage it or degrade its silastic seal.
Road Simulator
Avoid pressure-washing the transducer. Use only solvents that will not degrade the silastic seal.
Do not use high-pressure-air to clean debris from around the transducer connectors.
High-pressure-air can damage the silastic seals.
Use a fine wire brush and low air-pressure [0.07 MPa (10 psi)] to clean debris from around the transducer connectors.
Do not under-torque the lug nuts.
Lug nuts that are not properly tightened can become loose during testing. Loss of a wheel can cause damage to the test vehicle and transducer and result in injury to personnel.
Always tighten the lug nuts to the torque rating recommended for the vehicle/ wheel.
SWIFT 30 Sensors Installing the Transducer
99
Road Simulator
Equipment required This procedure requires one person. To install the transducer, you will need the
following equipment:
Hub adapter
Modified rim
Spindle housing adapter plate
Connector housing
Locating pins
Small set of hex-head wrenches (both English and metric)
Metric socket head drive set (up to 14 mm) with extension
Molykote g-n paste (MTS part number 011-010-207)
Bolts
For SWIFT 30A Transducer
48 size M10 X 1.5 mm
4 size M8 X 1.25 mm
8 size M5 X 0.8 mm
lug nuts
For SWIFT 30T Transducer
48 size M10 X 1.5 mm
4 size M8 X 1.25 mm
8 size M5 X 0.8 mm
Lug nuts
Torque wrenches, capable of the following ranges:
28–54 N•m (20–40 lbf•ft),
81–136 N•m (60-100 lbf•ft);
7 N•m (60 lbf •in)
Cables (transducer and BNC, plus customer-supplied from transducer
interface to data recorder)
Tie wraps
Installing the Transducer
100
Data recorder
12 V power supply (for example, a car battery)
SWIFT 30 Sensors
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