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LTD (RoyalTek). It is provided for the sole purpose of the business discussions
between supplier and RoyalTek and is covered under the terms of the
applicable Non-Disclosure Agreements. Disclosure of this information to other
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Prepared by RoyalTek Company LTD.
8F,256 Yang Guang Street, Neihu Chiu,Taipei, Taiwan, R.O.C.
20 Testability It shall be able to be tested by SiRF test II and single channel
22 Protocol setup It shall store the protocol setup in the SRAM memory.
23 DGPS 1.WAAS, EGNOS
Interface
24 LNA
25 I/O Pin 30pin stamp holes
It shall show C/No ≧ 37 dB-Hz when external power =
-130dBm.
28 dBHz (SSII normal version software)
28 dBHz (SSII ES version software)
16 dBHz (SSII XTrac version software)
33 dBHz (SSII ES version software)
32 dBHz (SSII XTrac version software)
33 dBHz (SSII ES version software)
28 dBHz (SSII XTrac version software)
75sec typical (SSII ES version software, Open sky)
45sec typical (SSII XTrac version software, Open sky)
40sec typical (SSII ES version software, Open sky)
35sec typical (SSII XTrac version software, Open sky)
18 sec. typical (SSII ES version software, Open sky)
4 sec. typical (SSII XTrac version software, Open sky)
≦ 200Hz in 60 sec
90000Hz≦Clock offset≦100000Hz
≦25m CEP.
Duty cycle ≦ 34%. (Variable)
Default: disable(option: enable)
It shall freeze the navigation update when speed ≦
2.5 km/hr
simulator.
2.RTCM protocol
On board LNA :
a. Gain ≧14dB
b. N.F. < 2dB
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REB-3300 Operational Manual
Mechanical requirements
26 Weight
Power consumption
27 Vcc DC 3.3 ±5%
28 Current REB3300:
29 Trickle power mode
30 Power down mode current 1. It means that the GPS receiver is in power down mode.
Environment
31 Operating temperature
32 Humidity
33 Interface Protocol 1. NMEA 0183 ver 3.0, GGA, GSA, RMC and GSV once per
Application Circuit
≦3.5g
Current ≦65mA@3.3V typical (w/o ext. antenna)
Average current ≦ 65mA. (IO float)
2. Current ≦800μA.
-40 ~ 85℃ ≦95%
2. SiRF Protocol
3. 4800 bps, 8 data bits, no parity, 1 stop bits
(1) Ground Planes:
REB-3300 GPS receiver needs two different ground planes. The GND_A pin(11、
12、13、14、15、16、18) shall be connect to analog ground.
The GND pin(2、10、30) connect to digital ground.
(2) Serial Interface:
The Serial interface pin(RXA、TX1、TXB、RXB) is recommended to pull up(10KΩ).
It can increase the stability of serial data.
(3) Backup Battery:
It’s recommended to connect a backup battery to V_BAT.
In order to enable the warm and hot start features of the GPS receiver. If you don’t
intend to use a backup battery, connect this pin to GND or open.
If you use backup battery, shall need to add a bypassing capacitor (10uF) at V_bat
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REB-3300 Operational Manual
trace. It can reduce noise and increase the stability.
(4) Antenna:
Connecting to the antenna has to be routed on the PCB. The transmission line must
to controlled impedance to connect RF_IN to the antenna or antenna connector of
your choice.
(5) Active antenna bias voltage:
The Vcc_RF pin(pin 20) is provide voltage 3.0V. If you use active antenna, you can
connect this pin to V_ANT_IN pin (pin 19) to provide bias voltage of active antenna.
The bias voltage will through RF_IN pin to provide active antenna bias voltage from
Vcc_RF pin.
If your bias voltage of active antenna isn’t 3.0V, you can input bias voltage to
V_ANT_IN pin(pin 19).And input bias voltage of you need. It can open if you use
passive antenna. The input bias voltage will through RF_IN pin to provide active
antenna bias voltage from V_ANT_IN pin.
The maximum power consumption of active antenna is about 100mW
(6) Power:
Connect Vcc pin to DC 3.3V.The power supply must add bypassing capacitor(10uF
and 1uF).It can reduce the Noise from power supply and increase power stability.
input
2 GND G Ground Digital Reference Ground
3 Bootselect I Boot mode
4 RXA I Serial port A
5 TXA O Serial port A
6 TXB O Serial port B
7 RXB I Serial port B
8 GPIO3 I/O General –purpose I/O
9 RF_ON O Indicates power state
of RF part
10 GND G Digital Ground Digital Reference Ground
11
GND_A G Analog Ground Analog Reference Ground
|
16
17 RF_IN I GPS Signal input 50 Ω @1.57542GHz
18 GND_A G Analog Ground Analog Reference Ground
19 V_ANT_IN I Active Antenna Bias
voltage
20 VCC_RF O Supply Antenna Bias
voltage
21 V_BAT I Backup voltage supply
22 Reset I Reset (Active low)
23 GPIO10 I/O General purpose I/O
DC +3.3V±10%
ILIH
ILIH
OLOH
OLOH
ILIH
≤≥
ILIH
≤≥
OLOH
OLOH
Receiving DC power supply for active antenna
bias.
±0.3
VV
0.3
O
3.6V~2.6 DC
≤
>
IH
IL
battery) (w/o10uA Current
VV
8.0 2.3V V
≤≥
ILIH
VVVV
4.0 4.2
≤≥
OLOH
VCCVVVCCVV
*3.0 *7.0≤≥
VCCVVVCCVV
*3.0 *7.0≤≥
VVVV
4.0 4.2≤≥
VVVV
4.0 4.2≤≥
VCCVVVCCVV
*3.0 *7.0≤≥
VCCVVVCCVV
*3.0 *7.0
VVVV
4.0 4.2
VVVV
0 85.2=
VCCVVVCCVV
*3.0 *7.0
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REB-3300 Operational Manual
24 GPIO6 I/O General purpose I/O
25 GPIO5 I/O General purpose I/O
26 GPIO7 I/O General purpose I/O
27 GPIO13 I/O General purpose I/O
28 GPIO15 I/O General purpose I/O
29 PPS O One pulse per second
30 GND G Digital Ground Digital Reference Ground
≤≥
ILIH
≤≥
OLOH
OLOH
Definition of Pin assignment
VCC(+3.3V DC power Input)
This is the main DC power supply input pin. It provides voltage to module.
GND
GND provides the ground for digital part.
VCCVVVCCVV
≤≥
ILIH
≤≥
OLOH
≤≥
ILIH
≤≥
OLOH
≤≥
ILIH
≤≥
OLOH
≤≥
ILIH
≤≥
OLOH
4.0 4.2
*3.0 *7.0
VVVV
4.0 4.2
*3.0 *7.0
VVVV
4.0 4.2
*3.0 *7.0
VVVV
4.0 4.2
*3.0 *7.0
VVVV
4.0 4.2
VCCVVVCCVV
*3.0 *7.0
VVVV
VVVV
4.0 4.2≤≥
VCCVVVCCVV
VCCVVVCCVV
VCCVVVCCVV
Bootselect
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_ON
This pin indicates state of RF voltage.
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
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REB-3300 Operational Manual
antenna(or antenna connector) has to be a controlled impedance line
(Microstrip at 50Ω).
V_ANT_IN
This pin is reserved an external DC power supply for active antenna.
If using 3.0V active antenna, pin 19 has to be connected to pin 20.
If using 3.3V or 12V active antenna ,this pin has to be connected to 3.3V or 5V
power supply.
VCC_RF
This pin provides DC voltage 3.0 for active antenna.
Reset
This pin provides an active-low reset input to the board. It causes the board to
reset and start searching for satellites. If not utilized, it may be left open.
PPS
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.
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 10uA.
Without an external backup battery or super cap, the TMP will execute a cold
start after every power on. To achieve the faster start-up offered by a hot or
warm start, either a battery backup must be connected or a super cap installed.
To maximize battery lifetime, the battery voltage should not exceed the supply
voltage and should be between 2.5V and 3.6V.
With the super cap (B1) installed, and after at least ten minutes of continuous
operation, the data retention is about seven hours.
Note that even though all other components are rated at –40 to +85 deg C , a
typical super cap is specified over a temperature range of –25 to +70 deg C and
a typical rechargeable Lithium battery is over –20 to +70 deg C.
GPIO Functions
Several I/Os are connected to the digital interface connector for custom
applications.
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REB-3300 Operational Manual
Test Software Specification
No Function Specification
1 Clock offset 88000Hz≦VAL≦104000Hz
2 Clock Drift VAL≦200Hz
3 C/No Hi Power Mean VAL≧38dB
4 C/No Hi Power Sigma VAL≦2dB
5 Bit Sync VAL≦5 Sec
6 Frame Sync VAL≦28 Sec
7 Phase Error
VAL≦0.22°
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REB-3300 Operational Manual
Software Interface
NMEA V3.0 Protocol
Its output signal level is TTL: 4800 bps (default), 8 bit data, 1 stop bit and no parity. It supports
the following NMEA-0183
Messages: GGA, GLL, GSA, GSV, RMC and VTG.
NMEA Output Messages: the Engine board outputs the following messages as shown in Table
1:
Table 1 NMEA-0183 Output Messages
NMEA Record Des cription
GGA Global positioning system fixed data
GLL Geographic position – latitude / longitude
GSA GNSS DOP and active satellites
GSV GNSS satellites in view
RMC Recommended minimum specific GNSS data
VTG Course over ground and ground speed
GGA-Global Positioning System Fixed Data
Table 2 contains the values of the following example:
$GPGGA, 161229.487, 3723.2475, N, 12158.3416, W, 1, 07, 1.0, 9.0, M, , , ,0000*18
Table 2 GGA Data Format
Name ExampleUnits Description
Message ID $GPGGAGGA protocol header
UTC Position 161229.487hhmmss.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 2-1
Satellites Used 07 Range 0 to 12
HDOP 1.0 Horizontal Dilution of Precision
MSL Altitude 9.0 meters
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REB-3300 Operational Manual
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
Table 3 Position Fix Indicator
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
GLL-Geographic Position –Latitude/Longitude
Table 3 contains the values of the following
Example: $GPGLL, 3723.2475, N, 12158.3416, W, 161229.487, A*2C
Table 3 GLL Data Format
Name ExampleUnitsDescription
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.ss
Status A A=data valid or V=data not valid
Checksum *2C
<CR><LF>
End of message termination
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REB-3300 Operational Manual
GSA-GNSS DOP and Active Satellites
Table 4 contains the values of the following example: