Detailed instructions for use are in the User's Guide.
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GR-86
GPS Engine Board
User's Guide
March 2, 2006 Version D
O UX
Technology Inc.
Fax: +886-3-6687111
1F, No. 30, R&D Rd. II, Hsinchu City 300, Science-based Industrial Park, Taiwan. Phone: +886-3-6687000
E-Mail: info@holux.com.tw Web: www.holux.com.tw All Right Reserved
HOLUX Technology, Inc. 1 1F, No.30, R&D Rd.II, Hsin-Chu City 300, Science-based Industrial Park, Taiwan TEL: 886-3-6687000 FAX: 886-3-6687111 E-mail:info@holux.com.tw Website:www.holux.com.tw
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TABLE OF CONTENTS
1. Introduction ..................................................................................................3 2. Main Feature................................................................................................3 3. Technical Specifications ...............................................................................4 3.1. Electrical Characteristics....................................................................4 3.2. Environmental Characteristics ...........................................................5 3.3. Physical Characteristics.....................................................................5 4. Software Interface........................................................................................6 4.1 NMEA Transmitted Messages.............................................................6 4.2 RTCM Received Data .......................................................................12 4.3 . Manufacturing Default.....................................................................13 5. Mechanical Dimensions .............................................................................14 5.1. GR-86 outline...................................................................................14 5.2 Pin assignment .................................................................................16 6. Operation and Test.....................................................................................17 Appendix A : Reference Design .....................................................................20 Appendix B: Ordering information ..................................................................20
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1. Introduction
HOLUX GR-86 Ver D is a high performance, low power consumption, small size, very easy integrated GPS module designed for a broad spectrum of OEM system applications. This product is based on the proven technology found in other HOLUX 20 channel GPS receivers and SiRF GSC3 chipset solution. The GPS module will track up to 20 satellites at a time while providing fast time-to-first-fix and one-second navigation updates. Its far reaching capability meets the sensitivity requirements of car navigation as well as other location-based applications. Therefore, HOLUX GR-86 module is very fit to the customers who devote themselves to AVL system integration and location-based service. The GR-86 design utilizes the latest surface mount technology (BGA) and high level circuit integration to achieve superior performance while minimizing space and power requirements. This hardware capability combined with software intelligence makes the board easy to be integrated and used in all kinds of navigation applications or products. The application system may communicate with the engine board set via CMOS 3V voltage level.
2. Main Feature
Build on high performance SiRF GSC3f chipset. Average Cold Start time and under 42 seconds. Low power consumption 20 channels "All-in-View" tracking. Integrated ARM7TDMI CPU with software engineering services and available for embedded customer defined applications. On chip 1Mb SRAM. On-board LNA and saw filter. Dual CMOS 3V serial ports with one for GPS receiver command message interface. Compact board size 24x24x3 mm for easy integration into hand-held device. Reacquisition Time 0.1 seconds Support Standard NMEA-0183 and SiRF Binary protocol Support Accurate 1PPS Output Signal Aligned with GPS Timing Multi-path Mitigation Hardware WAAS /EGNOS Demodulator
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3. Technical Specifications
3.1. Electrical Characteristics
3.1.1 General
1). FrequencyL1, 1575.42 MHz. 2). C/A code1.023 MHz chip rate. 3). Channels20
3.1.2 Accuracy (Open Sky)
1). Position10 meters, 2D RMS. 2). 7 meters 2D RMS, WAAS corrected. 3). 1-5 meters, DGPS corrected. 4). Time 1 microsecond synchronized to GPS time.
3.1.3 Datum
1). DefaultWGS-84. 2). Other Support different datum by request.
3.1.4 Acquisition Rate (Open sky, stationary requirements)
1). 2). 3). 4). Reacquisition0.1 sec., average. Hot start1 sec., average. Warm start38 sec., average. Cold start42 sec., average.
3.1.5 Dynamic Conditions
1). 2). 3). 4). Altitude : 18,000 meters (60,000 feet) Max Velocity515 m/s (1,000 knots) Max Acceleration4 G, Max Jerk20 meters/second, Max
3.1.6 Power
1). Input power input3.3~5.5VDC input 2). Input current: Less than 75 mA (without antenna)
3.1.7 RF interface
1). Minimum signal tracked: -159 dBm (based on GSC3f chip spec.)
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3.1.8 Serial Port
1). Two full duplex serial communication, CMOS 3V interface, with user selectable baud rate (4800-Default, 9600, 19200, 38400) 2). NMEA 0183 Version 2.2 ASCII output (GGA, GSA, GSV, RMC (VTG , GLL and ZDA for optional)) 3). SiRF binary-position, velocity, altitude, status output
3.1.9 TIMEMARK-1PPS Pulse
1). 2). 3). 4). Level CMOS 3V Pulse duration 1 usec Time reference at the pulse positive edge Measurements Aligned to GPS second, ±1 microsecond
3.2. Environmental Characteristics
1). Operating temperature range -20 to +70 2). Storage temperature range -40 to +85 .
3.3. Physical Characteristics
1) Active Size: 24(W) x 24(L) x 3(H) (mm) 2) Weight: less than 4 g
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4. Software Interface
The GR-86 interface protocol is based on the National Marine Electronics Association's NMEA 0183 ASCinterface specification, which is defined in NMEA 0183, Version 2.2 and the Radio Technical Commission for Maritime Services (RTCM Recommended Standards For Differential Navstar GPS Service, Version 2.1, RTCM Special Committee No.104). As soon as the initial self-test is complete, the GR-86 begins the process of satellite acquisition and tracking automatically. Under normal circumstances, it takes approximately 42 seconds to achieve a position fix, 38 seconds if ephemeris data is known. After a position fix has been calculated, information about valid position, velocity and time is transmitted over the output channel. The GR-86 utilizes initial data, such as last stored position, date, time and satellite orbital data, to achieve maximum acquisition performance. If significant inaccuracy exists in the initial data, or the orbital data is obsolete, it may take more time to achieve a navigation solution. The GR-86 Auto-locate feature is capable of automatically determining a navigation solution without intervention from the host system. However, acquisition performance can be improved as the host system initializes the GR-86 in the following situation:
4.1 NMEA Transmitted Messages
The default communication parameters for NMEA output are 4800 baud, 8 data bits, stop bit, and no parity. Table 4-1 NMEA-0183 Output Messages NMEA Record GPGGA GPGLL GPGSA GPGSV GPRMC GPVTG GPMSS GPZDA Description Global positioning system fixed data Geographic position- latitude/longitude GNSS DOP and active satellites GNSS satellites in view Recommended minimum specific GNSS data Course over ground and ground speed Radio-beacon Signal-to-noise ratio, signal strength, frequency, etc. PPS timing message (synchronized to PPS)
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4.1.1 Global Positioning System Fix Data (GGA)
Table 4-2 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
Table 4-2 GGA Data Format Name
Message ID UTC Time Latitude N/S Indicator Longitude E/W Indicator Position Fix Indicator Satellites Used HDOP MSL Altitude (1) Units Geoid Separation(1) Units Age of Diff. Corr. Diff. Ref. Station ID Checksum 0000 *18 End of message termination M
Example Units
Description
GGA protocol header hhmmss.sss ddmm.mmmm N=north or S=south dddmm.mmmm E=east or W=west See Table 5-3 Range 0 to 12 Horizontal Dilution of Precision
$GPGGA 161229.487 3723.2475 N 12158.3416 W 1 07 1.0 9.0 M Meters Meters Meters Meters
second Null fields when DGPS is not used
(1). SiRF Technology Inc. does not support geoid corrections. Values are WGS84 ellipsoid heights.
Table 4-3 Position Fix Indicator
Value Description
0 1 2 3
0 Fix not available or invalid GPS SPS Mode, fix valid Differential GPS, SPS Mode, fix valid GPS PPS Mode, fix valid
4.1.2 Geographic Position with Latitude/Longitude(GLL)
Table 4-4 contains the values for the following example:
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$GPGLL,3723.2475,N,12158.3416,W,161229.487,A*2C Table 4-4 GLL Data Format Name
Message ID Latitude N/S Indicator Longitude E/W Indicator UTC Position Status Checksum
Example
Units
Description
GLL protocol header ddmm.mmmm N/S Indicator N N=north or S=south dddmm.mmmm E=east or W=west hhmmss.sss A=data valid or V=data not valid End of message termination
$GPGLL 3723.2475 N 12158.3416 W 161229.487 A *2C
4.1.3 GNSS DOP and Active Satellites (GSA)
Table 4-5 contains the values for the following example: $GPGSA,A,3,07,02,26,27,09,04,15, , , , , ,1.8,1.0,1.5*33 Table 4-5 GSA Data Format Name
Message ID Mode 1 Mode 2 Satellite Used(1) Satellite Used(1) ...... Satellite Used(1) PDOP HDOP VDOP Checksum
1. Satellite used in solution.
Example
Units
Description
GSA protocol header See Table 5-6 See Table 5-7 Sv on Channel 1 Sv on Channel 2 .... Sv on Channel 12
$GPGSA A 3 07 02
1.8 1.0 1.5 *33
Position Dilution of Precision Horizontal Dilution of Precision Vertical Dilution of Precision End of message termination
HOLUX Technology, Inc. 8 1F, No.30, R&D Rd.II, Hsin-Chu City 300, Science-based Industrial Park, Taiwan TEL: 886-3-6687000 FAX: 886-3-6687111 E-mail:info@holux.com.tw Website:www.holux.com.tw
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Table 4-6 Mode 1
Value
M A
Manual--forced to operate in 2D or 3D mode 2DAutomatic--allowed to automatically switch 2D/3D
Table 4-7 Mode 2
Value Description
1 2 3
Fix Not Available 2D 3D
4.1.4 GNSS Satellites in View (GSV)
Table 4-8 contains the values for the following example:
$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 4-8 GSV Data Format Name
Message ID Number of Messages(1) Message Number(1) Satellites in View Satellite ID Elevation Azimuth SNR (C/No) .... Satellite ID Elevation Azimuth SNR (C/No) Checksum
Example Units
Description
GSV protocol header Range 1 to 3 Range 1 to 3 Channel 1 (Range 1 to 32)
$GPGSV 2 1 07 07 79 048 42 .... 27 27 138 42 *71
degrees Channel 1 (Maximum 90) degrees Channel 1 (True, Range 0 to 359) dBHz Range 0 to 99, null when not tracking Channel 4 (Range 1 to 32) degrees Channel 4 (Maximum 90) degrees Channel 4 (True, Range 0 to 359) dBHz Range 0 to 99, null when not tracking End of message termination
(1). Depending on the number of satellites tracked multiple messages of GSV data may be required.
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4.1.5 Recommended Minimum Specific GNSS Data (RMC)
Table 4-9 contains the values for the following example:
$GPRMC,161229.487,A,3723.2475,N,12158.3416,W,0.13,309.62,120598, ,*10
Table 4-9 RMC Data Format Name
Message ID UTC Time Status Latitude N/S Indicator Longitude E/W Indicator Speed Over Ground Course Over Ground Date Magnetic Variation(1) Checksum
directions.
Example
Units
Description
$GPRMC 161229.487 A 3723.2475 N 12158.3416 W 0.13 309.62 120598 *10 knots
RMC protocol header hhmmss.sss A=data valid or V=data not valid ddmm.mmmm N=north or S=south dddmm.mmmm E=east or W=west degrees True ddmmyy degrees E=east or W=west End of message termination
(1). SiRF Technology Inc. does not support magnetic declination. All "course over ground" data are geodetic WGS84
4.1.6 Course Over Ground and Ground Speed (VTG)
Table 4-10 contains the values for the following example: $GPVTG,309.62,T, ,M,0.13,N,0.2,K*6E Table 4-10 VTG Data Format Name
Message ID Course Reference Course
Example Units
Description
VTG protocol header
$GPVTG 309.62 T
degrees Measured heading True degrees Measured heading
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Reference Speed Units Speed Units Checksum
directions.
M 0.13 N 0.2 K *6E km/hr knots
Magnetic(1) Measured horizontal speed Knots Measured horizontal speed Kilometers per hour End of message termination
(1). SiRF Technology Inc. does not support magnetic declination. All "course over ground" data are geodetic WGS84
4.1.7 MSK Receiver Signal (MSS)
Table 4-11 contains the values for the following example: $GPMSS,55,27,318.0,100,*66 Table 4-11 MSS Data Format Name Message ID Signal Strength Signal-to-Noise Ratio Beacon Frequency Beacon Bit Rate
Checksum
Example Units
Description
protocol header dB SS of tracked frequency SNR of tracked frequency Currently tracked frequency 100 bits per second End of message termination
$GPMSS 55 27 318.0 100
66
MSS dB dB kHz
Note The MSS NMEA message can only be polled or scheduled using the MSK NMEA input message.
4.1.8 ZDA--SiRF Timing Message
Outputs the time associated with the current 1 PPS pulse. Each message will be output within a few hundred ms after the 1 PPS pulse is output and will tell the time of the pulse that just occurred. Table 4-12 contains the values for the following example: $GPZDA,181813,14,10,2003,00,00*4F
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Table 4-12 ZDA Data Format Name
Message ID UTC Time Day Month Year Local zone hour Local zone hour Checksum
Example Units
Description
ZDA protocol header Either using valid IONO/UTC or estimated from default leap seconds 01 TO 31 01 TO 12 1980 to 2079
$GPZDA 181813 14 10 2003 00 00 4F knots
Offset from UTC (set to 00) Offset from UTC (set to 00) End of message termination
4.2 RTCM Received Data
The default communication parameters for DGPS Input are 9600 baud, 8 data bits, stop bit, and no parity. Position accuracy of less than 5 meters can be achieved with the GPS-82 by using Differential GPS (DGPS) real-time pseudo-range correction data in RTCM SC-104 format, with message types 1,2, or 9. As using DGPS receiver with different communication parameters, GPS-82 may decode the data correctly to generate accurate messages and save them in battery-back SRAM for later computing.
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4.3 . Manufacturing Default
Parameter Input protocol Output protocol Baud rate Parity Stop bit Data bits Datum Protocol Com A NMEA NMEA 4800 None 1 8 WGS84 GGA,GSA,GSV,RMC or by demand Com B RTCM SC-104 None 9600 1 8
4.3.1 Setting Syntax
Datum change syntax: >DOS\Sirfprog /Fdataxx.dat Px Bx Csh1 -Px: x is com port, 1= COM1 2 = COM2 -Bx: Baud rate, 4800, 9600, 19200 or 38400 Example: Change Datum to WGS84, Sirfprog /Fdata58.dat P1 B4800 Csh1 After change datum, the new datum will keep in SRAM. If long time (more than 7 days) no power supplied to GR-86, user must resend datum to GR-86 when power on.
4.3.2 Addition Software
SiRFdemo is the Evaluation Receiver configuration and monitoring software provided with the GR-86. This software can be used to monitor real-time operation of the GR-86 Receiver, log data for analysis, upload new software to the Receiver, and configure the Receiver operation. See setup.pdf for more information on the use and operation of SiRFdemo software.
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5. Mechanical Dimensions
5.1. GR-86 outline
Picture
Outline Drawing
(8.5,24) (5,24) 3.5 mm. 0.2 mm. (0,21) (0,19) (0,17) (0,15) (0,13) (0,11) (0,9) (0,7) (0,5) (0,3) 1 20 (24,21) (24,19) (24,17) (24,15) (24,13) (24,11) (24,9) (24,7) (24,5) 10 11 (24,3)
1.5 mm.
24.0 mm.
(0,0) (16,0) 24.0 mm.
5.0 mm. (21,0)
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Recommend PCB layout
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5.2 Pin assignment
Table 5-1 is pin list of the 20-pin Interface Connector. Table 5-1
Pin 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 Pin Name GND RFIN GND GND NRESET LED_ONOFF BATTERY NSLEEP VCC_IN GND RXDB TXDA RXDA BOOT_SEL GND Type PWR Ground I RF signal input Function description
PWR Ground PWR Ground I O Reset, active low. Keep floating if not used. 1 HZ High/Low pulse output in tracking mode
PWR Backup battery input (2.53.3V) I Power down module, low active
PWR 3.3 ~ 5.5 VDC supply input PWR Ground I O I I Serial Data input B Serial Data Output A Serial Data Input A Pull high for firmware download mode. Keep NC if not used.
PWR Ground I I I O Reserve for future feature Reserve for future feature Reserve for future feature 1 µsec pulse per second when tracking
16 TIMER_SYNC 17 18 19 20 AMP_INTR FREQ_XFER TIMEMARK GND
PWR Ground
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6. Operation and Test
The customers can use HOLUX GPSView.exe to test the engine board. GPSViewer.exe is compatible with Microsoft Pocket PC or other operation system alike. 1). Install Microsoft ActiveSync to your PC, refer to your Pocket PC manual for installation procedure, as Fig. 6.1. 2). Setup your Pocket PC cradle to Desktop PC UART port. The Microsoft ActiveSync will detect your Pocket PC automatically. Setup your Pocket PC cradle to Desktop PC UART port. The Microsoft ActiveSync will detect your Pocket PC automatically, as Fig. 6.1.
(Fig. 6.1) 3). Double click the GPSViewer.exe on your PC, then Holux GPSViewer.exe program will install automatically, as Fig. 6.2.
(Fig. 6.2)
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4) Open "GPSViewer" on PC, as Fig. 6.3.
(Fig. 6.3) 5) The following window is show after executing 6) GPSViewer, as Fig. 6.4.
(Fig. 6.4) 7) Setup Baud rate: 4800, then push "Scan" bottom to scan your COM Port . Select your COM Port (COM1 ~ COM10), then push "Open GPS" bottom, as Fig. 6.5, Fig. 6.6, and Fig. 6.7.
(Fig. 6.5)
(Fig. 6.6)
(Fig. 6.7)
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8)
Select "GPS Status" to show the satellite diagram like below, as Fig. 6.8.
(Fig. 6.8)
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Appendix A : Reference Design
Fig A-1 is GR-86 connects to RS-232 transceiver solutions intended for portable or hand-held applications such as notebook and palmtop computers.
VCC 1 2 4 5 6 13 12 15 10 1 14 20 C4 0.1uF U1 SP3223EEA-SSOP20 19 C1+ VCC C1C2+ C2T1_TTL T2_TTL R1_TTL R2_TTL EN ON OFF V+ VT1_232 T2_232 R1_232 R2_232 INVALID GND 3 7 17 8 16 9 11 18 VCC 1 1 1 C1 0.1uF 2
12
VCC_IN(9)
GND(10)
C2 0.1uF C3 0.1uF TXDA
GND CON/DB9/90D/F 11 1 6 2 7 3 8 4 9 5 10 J26 GND
GND(3) RFIN(2) GND(1)
TXDA(12) RXDA(13) RXDB(11)
2
Antenna
C5 0.1uF 2 C6 0.1uF 2 GND
RXDA RXDB VCC 1
DGPSIN
GR-86 engine board
GND
GND
GND
2
GND
(Fig A-1)
Appendix B: Ordering information
Model No. GR-86-A GR-86-B Chipset GSC3f GSC3f RF interface output voltage (V) RF antenna power 2.8 VDC from GR-86 RF antenna power supply from VCC_IN
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