GlobalSat ET-318 User Guide

Page 1
ET-318
GPS Engine Board ET-318
Version 2.0
07/19/2007
Globalsat Technology Corporation Headquarters (Far East Century Park)
16F., No. 186, Jian-Yi Road, Chung-Ho City, Taipei Hsien 235, Taiwan
Tel: 886-2-8226-3799/ Fax: 886-2-8226-3899
E-mail : service@globalsat.com.tw
Website: www.globalsat.com.tw
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ET-318
1. Product Information
Product Name: ET-318
Product Description:
ET-318 is a compact, high performance, and low power consumption GPS engine board. It uses SiRF
Star III chipset which can track up to 20 satellites at a time and perform fast TTFF in weak signal
environments. ET-318 is suitable for the following applications:
Automotive navigation
Personal positioning
Fleet management
Mobile phone navigation
Marine navigation
Product Features:
SiRF star III high performance GPS Chipset
Very high sensitivity (Tracking Sensitivity: -159 dBm)
Extremely fast TTFF (Time To First Fix) at low signal level
Two serial ports
Built-in LNA
Compact size (15.2mm * 14 mm * 2.6mm) suitable for space-sensitive application
One size component, easy to mount on another PCB board
Support NMEA 0183 and SiRF binary protocol
Product Specifications
GPS Receiver
Chipset
Frequency L1, 1575.42 MHz
Code C/A Code
Protocol NMEA 0183 v2.2
SiRF GSC3f/LP
Default:GGA,GSA,GSV,RMC
Support:VTG,GLL,ZDA)
SiRF binary and NMEA Command
Available Baud Rate 4,800 to 57,600 bps adjustable
Channels 20
The Specifications are subject to be changed without notice. Copyright © 2007, GlobalSat Technology.
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Flash 4Mbit
Sensitivity Tracking:-159dBm
Cold Start 42 seconds, average
Warm Start 38 seconds, average
Hot Start 1 second, average
Reacquisition 0.1 second, average
Accuracy Position: 10 meters, 2D RMS
Velocity: 0.1 m/s
Time: 1us synchronized to GPS time
ET-318
5 meters, 2D RMS, WAAS enabled
Maximum Altitude
Maximum Velocity
Maximum Acceleration
Update Rate 1 Hz
DGPS WAAS, EGNOS, MSAS
Datum WGS-84
I/O Pins 2 serial ports
Type 17-pin stamp holes
Dimensions 15.2 mm * 14 mm * 2.6 mm
Power Supply
Backup Voltage
Power Consumption
18,000 meter
515 meter/second
4G
Interface
Physical Characteristic
DC Characteristics
3.3Vdc ± 5%
2.0 ~ 3.6Vdc ± 10%
Acquisition: 42mA Tracking: 25mA
Environmental Range
Humidity Range 5% to 95% non-condensing
Operation Temperature
Storage Temperature
-40℃ to 85℃
-40℃ to 125℃
The Specifications are subject to be changed without notice. Copyright © 2007, GlobalSat Technology.
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ET-318
2. Technical Information
Block Diagram
The Specifications are subject to be changed without notice. Copyright © 2007, GlobalSat Technology.
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Module Pin Assignment:
ET-318
Pin
1 GND G Analog Ground
2 RF_IN RF GPS Signal input
3 GND G Analog Ground
4 NRESET I Reset (Active low)
5 VCC_IN PWR DC Supply Voltage input
6 VBAT PWR Backup voltage supply
7 RXB I Serial port B
8 TXB O Serial port B
9 GND G Analog Ground
10 BOOTSEL Boot mode
11 TXA O Serial port A
12 RXA I Serial port A
13 GPIO1 I General –purpose I/O
14 GPIO14 I General –purpose I/O
15 TIMEMARK O One pulse per second
16 GPIO13 I General –purpose I/O
17 GPIO15 I General –purpose I/O
Signal Name
I/O
Description
The Specifications are subject to be changed without notice. Copyright © 2007, GlobalSat Technology.
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Definition of Pin assignment
ET-318
VCC_IN
This is the main DC supply for a 3.3V +- 5% DC input power module board.
GND
GND provides the ground for digital part.
BOOTSEL
Set this pin to high for programming flash.
RXA
This is the main receiver channel and is used to receive software commands to the board from SIRFdemo software or from user written software. PS: Pull up if not used.
RXB
This is the auxiliary receiving channel and is used to input differential corrections to the board to enable DGPS navigation. PS: Pull up if not used.
TXA
This is the main transmitting channel and is used to output navigation and measurement data to SiRFdemo or user written software.
TXB
For user’s application (not currently used).
RF_IN
This pin receiver signal of GPS analog .due to the RF characteristics of the signal the design has to certain criteria. The line on the PCB from the antenna(or antenna connector) has to be a controlled microstrip line at 50Ω.
Backup battery (V_BAT)
This is the battery backup input that powers the SRAM and RTC when main power is removed. Typical current draw is 15uA. Without an external backup battery, the module/engine board will execute a cold star after every turn on. To achieve the faster start-up offered by a hot or warm start, a battery backup must be connected. The battery voltage should be between 2.0v and 5.0v.
TIMEMARK
This pin provides one pulse-per-second output from the board, which is synchronized to GPS time. This is not available in Trickle Power mode.
GPIO Functions
Several I/Os are connected to the digital interface connector for custom applications.
The Specifications are subject to be changed without notice. Copyright © 2007, GlobalSat Technology.
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Application Circuit
ET-318
GPS Active Antenna Specification(Recommendation)
Frequency: 1575.42+2 MHz
Axial Ratio: 3 dB Typical
output Impedance: 50
Polarization: RHCP
Amplifier Gain :18~22dB Typical
Output VSWR: 2.0 Max.
Noise Figure: 2.0 dB Max
The Specifications are subject to be changed without notice. Copyright © 2007, GlobalSat Technology.
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Dimensions
ET-318
Recommend Layout PAD
The Specifications are subject to be changed without notice. Copyright © 2007, GlobalSat Technology.
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ET-318
Application Circuit
1.
J1_I-PEX connect
External antenna
1 2
50 Ohm Micro strip line
RF Switch
2
2
1
GPS_3V3
C1
1 2
1U
24-20003-12030N
C2
0.1U
1 2
ET318 Application guideline
VCC-R F
12
L1
33N
50 Ohm Micro strip line
1
D5
RB521S
1 2
12
R1 270R
BATTERY
BT1
C3
100p
12
D6
RB512S
RESET
RXB
TXB
1
2
3
4
5
6
7
8
U1
GND
RF_I N
GND
NRESET
VCC_I N
VBAT
RXB
TXB
GPS
GPIO15
GPIO13
TIMEMARK
GPIO14
BOOTSEL
GPIO1
RXA
TXA
GND
17
16
TIMEMAR K
15
14
13
12
11
10
9
GPIO15
GPIO13
GPIO14
GPIO1
RXA
TXA
Bootsel
L4 BLM18AG121SN1D
L3 BLM18AG121SN1D
12
12
TXD 1
RXD1
2.
GPS_3V3
1 2
VCC-R F
J1_I-PEX connec t
External antenna
1 2
50 Ohm Micro strip line
50 Ohm Micro strip line
RF Switch Circuit
C1
1U
C2
0.1U
1 2
D5
RB521S
12
L1
1 2
12
33N
R1 270R
BATTERY
BT1
C3
100p
RB512S
12
RESET
RXB
D6
TXB
1
2
3
4
5
6
7
8
U1
GND
RF_I N
GND
NRESET
VCC_I N
VBAT
RXB
TXB
GPS
GPIO15
GPIO13
TIMEMAR K
GPIO14
GPIO1
RXA
TXA
BOOTSEL
GND
17
16
TIMEMARK
15
14
13
12
11
10
9
GPIO15
GPIO13
GPIO14
GPIO1
RXA
TXA
Bootsel
L4 BLM18AG121SN1D
L3 BLM18AG121SN1D
12
12
TXD 1
RXD1
The Specifications are subject to be changed without notice. Copyright © 2007, GlobalSat Technology.
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3.GPS Power
VCC
GPS-power
ET-318
GPS_3V3
GPS_3V3
12
C4
+
22uF/10V
U1
1
VINNCVOUT
4
XC6209F332MRN
CE
GND
5 3 2
R2 100K
1 2
12
C5
1uF /2 5V
L2
GMLB-100505-0020P-N8
12
C6
470pF
GPIO
C7
10uF/16V
12
12
+
C8
0.1uF
Layout Rule
.Do not routing the other signal or power trace under the engine board .
* RF:
This pin receives signal of GPS analog via external active antenna .It has to be a has to be a
controlled impedance at 50 ohm .
Do not have RF traces closed the other signal path and routing it on the top layer.
Keep the RF traces as short as possible
* Antenna: Keep the active antenna on the top of your system and confirm the antenna radiation patternaxial
ratiopower gainnoise figureVSWR are correct when you Setup the antenna in you case.
GPS Passive (or Active )Antenna Specification(Recommendation)
Frequency: 1575.42±2 MHz
Axial Ratio: 3 dB Typical
output Impedance: 50
Polarization: RHCP
Output VSWR: 1.5 Max.
Active option
Low Noise Amplifter:
Amplifier Gain :18~22dB Typical
Output VSWR: 2.0 Max.
Noise Figure: 2.0 dB Max.
The Specifications are subject to be changed without notice. Copyright © 2007, GlobalSat Technology.
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ET-318
Definition of Pin assignment
VCC_IN
This is the main DC supply for a 3.3V ± 5% DC input power module board.
GND
GND provides the ground for digital part.
BOOTSEL
Set this pin to high for programming flash.
RXA
This is the main receive channel for receiving software commands to the engine board from
SiRFdemo software or from user written software.
Option to add EMI solutions
RXB
This is the auxiliary receiving channel and is used to input differential corrections to the board to
enable DGPS navigation.
PS: Pull up if not used.
TXA
This is the main transmits channel for outputting navigation and measurement data to user’s
navigation software or user written software.
Output TTL level, 0V ~ 2.85V
Option to add EMI solutions
TXB
For user’s application (not currently used).
RF_IN
This pin receives signal of GPS analog via external active antenna .It has to be a has to be a
controlled impedance at 50 ohm .Do not have RF traces closed the other signal path and routing it
on the top layer.
Keep the RF traces as short as possible.
TIMEMARK
This pin provides one pulse-per-second output from the board, which is synchronized to GPS time.
This is not available in Trickle Power mode.
The Specifications are subject to be changed without notice. Copyright © 2007, GlobalSat Technology.
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ET-318
Backup battery (V_BAT)
This is the battery backup input that powers the SRAM and RTC when main power is removed.
Typical current draw is 15uA. Without an external backup battery, the module/engine board will
execute a cold star after every turn on.
To achieve the faster start-up offered by a hot or warm start, a battery backup must be connected.
The battery voltage should be between 2.0v and 5.0v.
GPIO Functions
Several I/Os are connected to the digital interface connector for custom applications.
(For example, on/off LED)
Other
VCC_RF:
This is providing bias voltage for active antenna via a inductance.
The Specifications are subject to be changed without notice. Copyright © 2007, GlobalSat Technology.
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ET-318
ET-318 Demo Kit Test Description
Test Board Connection ET-318 Demo Kit:
Demo Kit J2 (Male) Connection Test Board J5 (Female)
Definition of Pin assignment
J2: J3:
Pin Signal Name Pin Signal Name Pin Signal Name Pin Signal Name
1 VCC 2 VCC 1 GPIO15 2 NC
3 NC 4 NC 3 GPIO13 4 NC
5 NC 6 NC 5 TIMEMARK 6 NC
7 NC 8 NC 7 GPIO14 8 NC
9 NC 10
The Specifications are subject to be changed without notice. Copyright © 2007, GlobalSat Technology.
GND 9 GPIO1 10
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NC
Page 14
ET-318
11
13
15
17
19
TXA 12
GND 14
RXB 16
NC 18
NC 20
RXA 11
TXB 13
GND 15
GND 17
NC 19
JP1: VBAT
JP2: Active Antenna VCC
JP3: Bootsel
Test Software GPSinfo:
1. Select COM Port & Baud Rate
2. Press Start GPS
RESET 12
NC 14
NC 16
NC 18
NC 20
NC
NC
NC
NC
NC
The Specifications are subject to be changed without notice. Copyright © 2007, GlobalSat Technology.
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SOFTWARE COMMAND
Name
Example
Units
Description
Message ID
$GPGGA
GGA protocol he
ader
UTC Time
161229.487
hhmmss.sss
Latitude
3723.2475
ddmm.mmmm
N/S Indicator
N N=north or S=south
Longitude
12158.3416
dddmm.mmmm
E/W Indicator
W E=east or W=west
Position Fix Indicator
1 See Table B
-3
Satellites Used
07 Range 0 to 12
HDO
P 1.0
Horizontal Dilution of Precision
MSL Altitude
9.0 meters
Units
M
meters
Geoid Separation
meters
Units
M
meters
Age of Diff. Corr.
second
Null fields when DGPS is not used
Diff. Ref. Station ID
0000
Checksum
*18
<CR><LF>
End of
message termination
Value
Description
0 Fix not available or invalid
1 GPS SPS Mode, fix valid
2 Differential GPS
, SPS Mode , fix valid
3 GPS PPS Mode, fix valid
NMEA Output Command
GGA-Global Positioning System Fixed Data
ET-318
Table B-2 contains the values for the following example:
$GPGGA,161229.487,3723.2475,N,12158.3416,W,1,07,1.0,9.0,M,,,,0000*18
1
1
Table B-2 GGA Data Format
SiRF Technology Inc. does not support geoid corrections. Values are WGS84 ellipsoid heights.
Table B-3 Position Fix Indicator
GLL-Geographic Position-Latitude/Longitude
$GPGLL,3723.2475,N,12158.3416,W,161229.487,A*2C
The Specifications are subject to be changed without notice. Copyright © 2007, GlobalSat Technology.
Table B-4 contains the values for the following example:
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Name
Example
Units
Description
Message ID
$GPGLL
GLL protocol header
Latitude
3723.2475
ddmm.mmmm
N/S Indicator
n N=north or S=south
Longitude
12158.3416
dddmm.mmmm
E/W Indicator
W E=east or W=west
UTC Position
161229.487
hhmmss.sss
Status
A A=data valid or V=data not valid
Checksum
*2C
<CR><LF>
End of message termination
Table B-4 GLL Data Format
GSA-GNSS DOP and Active Satellites
$GPGSA,A,3,07,02,26,27,09,04,15,,,,,,1.8,1.0,1.5*33
Table B-5 GSA Data Format
Table B-5 contains the values for the following example:
Name Example Units Description Message ID $GPGSA Mode1 A See Table B-6 Mode2 3 See Table B-7 Satellite Used1 07 Sv on Channel 1 Satellite Used1 02 Sv on Channel 2 ….. Satellite Used1 Sv on Channel 12 PDOP 1.8 Position dilution of Precision HDOP 1.0 Horizontal dilution of Precision VDOP 1.5 Vertical dilution of Precision Checksum *33 <CR><LF> End of message termination
Table B-6 Mode1
Value
M Manual-forced to operate in 2D or 3D mode A 2Dautomatic-allowed to automatically switch 2D/3D
Table B-7 Mode 2
Value
1 Fix Not Available 2 2D 3 3D
GSV-GNSS Satellites in View
1. Satellite used in solution.
Description
Description
GSA protocol header
ET-318
The Specifications are subject to be changed without notice. Copyright © 2007, GlobalSat Technology.
Table B-8 contains the values for the following example:
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Name
Example
Description
Message ID
$GPGSV
GSV protocol header
Number of Messages
2 Range 1 to 3
Message Number
1 Range 1 to 3
Satellites in View
07
Satellite ID
07 Channel 1(Range 1 to 32)
Elevation
79
degree
s Channel 1(Maximum90)
Azimuth
048 degrees
Channel 1(True, Range 0 to 359)
SNR(C/No)
42
dBHz
Range 0 to 99,null when not tracking
…….
…….
Satellite ID
27 Channel 4 (Range 1 to 32)
Elevation
27
Degrees
Channel 4(Maximum90)
Azimuth
138 Degrees
Chann
el 4(True, Range 0 to 359)
SNR(C/No)
42
dBHz
Range 0 to 99,null when not tracking
Checksum
*71
<CR><LF>
End of message termination
Name
Example
Units
Descript
ion
Message ID
$GPRMC
RMC protocol header
UTC Time
161229.487
hhmmss.sss
Status
A A=data valid or V=data not valid
Latitude
3723.2475
ddmm.mmmm
N/S Indicator
N N=north or S=south
Longitude
12158.3416
dddmm.mmmm
E/W Indicator
W E=east or W=
west
Speed Over Ground
0.13 knots
Course Over Ground
309.62
degrees
True
Date
120598
ddmmyy
Magnetic Variation
degrees
E=east or W=west
Checksum
*10
<CR><LF>
End of message termination
$GPGSV,2,1,07,07,79,048,42,02,51,062,43,26,36,256,42,27,27,138,42*71
$GPGSV,2,2,07,09,23,313,42,04,19,159,41,15,12,041,42*41
Table B-8 GSV Data Format
1
1
ET-318
Depending on the number of satellites tracked multiple messages of GSV data may be required.
$GPRMC,161229.487,A,3723.2475,N,12158.3416,W,0.13,309.62,120598,,*10
Table B-10 RMC Data Format
RMC-Recommended Minimum Specific GNSS Data
Table B-10 contains the values for the following example:
2
SiRF Technology Inc. does not support magnetic declination. All “course over ground” data are
geodetic WGS48 directions.
The Specifications are subject to be changed without notice. Copyright © 2007, GlobalSat Technology.
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Name
Example
Units
Description
Message ID
$GPVTG
VTG protocol header
Course
309.62
degrees
Measur
ed heading
Reference
T True
Course
degrees
Measured heading
Reference
M Magnetic
Speed
0.13 knots
Measured horizontal speed
Units
N Knots
Speed
0.2 Km/hr
Measured horizontal speed
Units
K Kilometers per hour
Checksum
*6E
<CR><LF>
End of
message termination
ET-318
VTG-Course Over Ground and Ground Speed
$GPVTG,309.62,T,,M,0.13,N,0.2,K*6E
2.2 NMEA Input Command
A)
. Set Serial Port ID:100 Set PORTA parameters and protocol
This command message is used to set the protocol(SiRF Binary, NMEA, or USER1) and/or the
communication parameters(baud, data bits, stop bits, parity). Generally,this command would be used to
switch the module back to SiRF Binary protocol mode where a more extensive command message set is
available. For example,to change navigation parameters. When a valid message is received,the parameters
will be stored in battery backed SRAM and then the receiver will restart using the saved parameters.
Format:
$PSRF100,<protocol>,<baud>,<DataBits>,<StopBits>,<Parity>*CKSUM
<CR><LF>
The Specifications are subject to be changed without notice. Copyright © 2007, GlobalSat Technology.
<protocol> 0=SiRF Binary, 1=NMEA, 4=USER1
<baud> 1200, 2400, 4800, 9600, 19200, 38400
<DataBits> 8,7. Note that SiRF protocol is only valid f8 Data bits
<StopBits> 0,1
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<Parity> 0=None, 1=Odd, 2=Even
Example 1: Switch to SiRF Binary protocol at 9600,8,N,1
$PSRF100,0,9600,8,1,0*0C<CR><LF>
Example 2: Switch to User1 protocol at 38400,8,N,1
$PSRF100,4,38400,8,1,0*38<CR><LF>
**Checksum Field: The absolute value calculated by exclusive-OR the 8 data bits of
each character in the Sentence,between, but excluding “$” and “*”. The
hexadecimal value of the most significant and least significant 4 bits of the result are
convertted to two ASCII characters (0-9,A-F) for transmission. The most
significant character is transmitted first.
**<CR><LF> : Hex 0D 0A
ET-318
B). Navigation lnitialization ID::101 Parameters required for start
This command is used to initialize the module for a warm start, by providing current position in X, Y, Z coordinates),clock offset, and time. This enables the receiver to search for the correct satellite signals at
the correct signal parameters. Correct initialization parameters will enable the receiver to acquire signals
more quickly, and thus, produce a faster navigational solution.
When a valid Navigation Initialization command is received, the receiver will restart using the input
parameters as a basis for satellite selection and acquisition.
Format::
$PSRF101,<X>,<Y>,<Z>,<ClkOffset>,<TimeOfWeek>,<WeekNo>,<chnlCount>,<ResetCfg>
*CKSUM<CR><LF>
<X> X coordinate position
INT32
<Y> Y coordinate position
INT32
<Z> Z coordinate position
INT32
The Specifications are subject to be changed without notice. Copyright © 2007, GlobalSat Technology.
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<ClkOffset> Clock offset of the receiver in Hz, Use 0 for last saved value
if available. If this is unavailable, a default value of 75000
for GSP1, 95000 for GSP 1/LX will be used.
INT32
<TimeOf Week> GPS Time Of Week
UINT32
<WeekNo> GPS Week Number
UINT16
ET-318
Week No and Time Of Week calculation from UTC time
<chnlCount> Number of channels to use.1-12. If your CPU throughput
is not high enough, you could decrease needed
throughput by reducing the number of active channels
UBYTE
<ResetCfg> bit mask
0×01=Data Valid warm/hotstarts=1
0×02=clear ephemeris warm start=1
0×04=clear memory. Cold start=1
UBYTE
The Specifications are subject to be changed without notice. Copyright © 2007, GlobalSat Technology.
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ET-318
Example: Start using known position and time.
PSRF101,-2686700,-4304200,3851624,96000,497260,921,12,3*7F
C). Set DGPS Port ID:102 Set PORT B parameters for DGPS input
C). Set DGPS Port ID:102 Set PORT B parameters for DGPS input
C). Set DGPS Port ID:102 Set PORT B parameters for DGPS inputC). Set DGPS Port ID:102 Set PORT B parameters for DGPS input
This command is used to control Serial Port B that is an input only serial port
used to receive
RTCM differential corrections.
Differential receivers may output corrections using different
communication parameters. The default
communication parameters for PORT B are 9600
Baud, 8data bits, 0 stop bits, and no parity. If a DGPS receiver
is used which has different communication parameters, use this command to allow the receiver to
correctly decode the data. When a valid message is received, the parameters will be stored in
battery backed SRAM and then the receiver will restart using the saved parameters.
Format:
PSRF102,<Baud>,<DataBits>,<StopBits>,<Parity>*CKSUM<CR><LF>
<baud> 1200,2400,4800,9600,19200,38400
<DataBits> 8
<StopBits> 0,1
The Specifications are subject to be changed without notice. Copyright © 2007, GlobalSat Technology.
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ET-318
<Parity> 0=None,Odd=1,Even=2
Example: Set DGPS Port to be 9600,8,N,1
PSRF102,9600,8,1.0*12
D). Query/Rate Control ID:103 Query standard NMEA message and/or set output rate
D). Query/Rate Control ID:103 Query standard NMEA message and/or set output rate
D). Query/Rate Control ID:103 Query standard NMEA message and/or set output rateD). Query/Rate Control ID:103 Query standard NMEA message and/or set output rate
This command is used to control the output of standard NMEA message GGA, GLL, GSA,
GSV
RMC, VTG. Using this command message, standard NMEA message may be polled once,
or setup for periodic output. Checksums may also be enabled or disabled depending
on the needs of the receiving program. NMEA message settings are saved in battery
backed memory for each entry when the message is accepted.
Format:
PSRF103,<msg>,<mode>,<rate>,<cksumEnable>*CKSUM<CR><LF>
<msg> 0=GGA,1=GLL,2=GSA,3=GSV,4=RMC,5=VTG
<mode> 0=SetRate,1=Query
<rate> Output every <rate>seconds, off=0,max=255
<cksumEnable> 0=disable Checksum,1=Enable checksum for specified
message
Example 1: Query the GGA message with checksum enabled
The Specifications are subject to be changed without notice. Copyright © 2007, GlobalSat Technology.
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ET-318
PSRF103,00,01,00,01*25
Example 2: Enable VTG message for a 1Hz constant output with checksum enabled
PSRF103,05,00,01,01*20
Example 3: Disable VTG message
PSRF103,05,00,00,01*21
E). LLA Navigation lnitialization ID:104 Parameters required to start using Lat/Lon/Alt
E). LLA Navigation lnitialization ID:104 Parameters required to start using Lat/Lon/Alt
E). LLA Navigation lnitialization ID:104 Parameters required to start using Lat/Lon/Alt E). LLA Navigation lnitialization ID:104 Parameters required to start using Lat/Lon/Alt
This command is used to initialize the module for a warm start, by providing current position (in
Latitude, Longitude, Altitude coordinates), clock offset, and time. This enables the receiver
to search for the correct satellite signals at the correct signal parameters. Correct initialization
parameters will enable the receiver to acquire signals more quickly, and thus, will produce a
faster navigational soution.
When a valid LLANavigationInitialization command is received,the receiver will restart using the
input parameters as a basis for satellite selection and acquisition.
Format:
PSRF104,<Lat>,<Lon>,<Alt>,<ClkOffset>,<TimeOfWeek>,<WeekNo>,
<ChannelCount>, <ResetCfg>*CKSUM<CR><LF>
<Lat> Latitude position, assumed positive north of equator and negative south of
The Specifications are subject to be changed without notice. Copyright © 2007, GlobalSat Technology.
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ET-318
equator float, possibly signed
<Lon> Longitude position, it is assumed positive east of Greenwich
and negative west of Greenwich
Float, possibly signed
<Alt> Altitude position
float, possibly signed
<ClkOffset> Clock Offset of the receiver in Hz, use 0 for last saved value if available. If
this is unavailable, a default value of 75000 for GSP1, 95000 for GSP1/LX
will be used.
INT32
<TimeOfWeek> GPS Time Of Week
UINT32
<WeekNo> GPS Week Number
UINT16
<ChannelCount> Number of channels to use. 1-12
UBYTE
<ResetCfg> bit mask 0×01=Data Valid warm/hot starts=1
0×02=clear ephemeris warm start=1
The Specifications are subject to be changed without notice. Copyright © 2007, GlobalSat Technology.
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ET-318
0×04=clear memory. Cold start=1
UBYTE
Example: Start using known position and time.
PSRF104,37.3875111,-121.97232,0,96000,237759,922,12,3*37
F). Development Data On/Off ID:105 Switch Development Data Messages On/Off
F). Development Data On/Off ID:105 Switch Development Data Messages On/Off
F). Development Data On/Off ID:105 Switch Development Data Messages On/Off F). Development Data On/Off ID:105 Switch Development Data Messages On/Off
Use this command to enable development debug information if you are having trouble getting
commands accepted. Invalid commands will generate debug information that should
enable the user to determine the source of the command rejection. Common reasons for
input command rejection are invalid checksum or parameter out of specified range. This setting is
not preserved across a module reset.
Format: PSRF105,<debug>*CKSUM<CR><LF>
<debug> 0=Off,1=On
Example: Debug On PSRF105,1*3E
Example: Debug Off PSRF105,0*3F
GGGG).
). Select Datum
Select Datum ID:10
). ).
Select DatumSelect Datum
Transformations
Transformations
TransformationsTransformations
ID:106666
ID:10 ID:10
Selection of datum to be used for coordinate
Selection of datum to be used for coordinate
Selection of datum to be used for coordinateSelection of datum to be used for coordinate
GPS receivers perform initial position and velocity calculations using an earth-centered earth-fixed
(ECEF) coordinate system. Results may be converted to an earth model (geoid) defined by the
selected datum. The default datum is WGS 84 (World Geodetic System 1984) which provides a
The Specifications are subject to be changed without notice. Copyright © 2007, GlobalSat Technology.
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worldwide common grid system that may be translated into local coordinate systems or map datums.
(Local map datums are a best fit to the local shape of the earth and not valid worldwide.)
Examples:
Datum select TOKYO_MEAN
$PSRF106,178*32
ET-318
The Specifications are subject to be changed without notice. Copyright © 2007, GlobalSat Technology.
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