Global Sat ET-332 User manual

環天衛星科技股份有限公司
PRODUCT USER MANUAL
GPS ENGINE BOARD
ET-332
GlobalSat Technology Corporation
台北縣中和市建一路 186 號 16 樓 ( 遠東世紀廣場 )
16, No.186,Chien 1Road, 235Chung Ho City,Taipei Hsien, Taiwan ,R.O.C.
Tel: [phone](Rep.) Fax: [phone]
Web: www.globalsat.com.tw E-mail: [email protected]

Features:
SiRF starⅢhigh performance GPS Chip Set
Very high sensitivity (Tracking Sensitivity: -159 dBm)
Extremely fast TTFF (Time To First Fix) at low signal level
Compact size (40.5mm * 35 mm * 10mm) suitable for space-sensitive application
Support NMEA 0183 and SiRF binary protocol
Build-in SuperCap to reserve system data for rapid satellite acquisition.
Cold start under 40seconds, average
Hot start under 1seconds, average
Specification:
General
Chipset SiRF StarⅢ
Frequency L1, 1575.42 MHz
C/A code 1.023 MHz chip rate
Channels 20 channel all-in-view tracking
Sensitivity -159 dBm
Accuracy
Position 10 meters, 2D RMS
5 meters, 2D RMS, WAAS enabled
Velocity 0.1 m/s
Time 1us synchronized to GPS time
Datum
Default WGS-84
Acquisition Time
Reacquisition 0.1 sec., average
Hot start 1 sec., average
Warm start 38 sec., average
Cold start 42 sec., average
Dynamic Conditions
Altitude 18,000 meters (60,000 feet) max
Velocity 515 meters /second (1000 knots) max

Acceleration Less than 4g
Jerk 20m/sec **3
Power
Main power input 3.8V ~ 6.5V DC input
Power consumption 75mA (Continuous mode)
30mA (Trickle power mode)
Interface
Baud rate 4,800 to 57,600 bps adjustable
Output message SiRF binary or
NMEA 0183 GGA, GSA, GSV, RMC, VTG, GLL
Environmental
Operating Temp -40℃to +85℃

Physical Characteristics

Interface Connection
* Pin-out of the 12-pin interface connector
Pin
Number Name Description Type
1 GND Ground
2 VBAT Backup Battery Input
3 VDC 3.8V~5.5V DC Power Input Input
4 PBRES Push Button Reset Input (Active Low) Input
5 GPIO1 (Reserved)
6 TXA Serial Data Output A (GPS Data) Output
7 RXA Serial Data Input A (Command) Input
8
GND Ground
9 GND Ground
10 SELECT (Reserved)
11 TIMEMARK 1PPS Time Mark Output Output
12 GND Ground
Interface description
* VDC (DC power input):
This is the main DC supply for a 3.8V ~ 5.5V power module board.
* VBAT (Backup battery):
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,
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. To
maximize battery lifetime, the battery voltage should be between 2.5v and 3.6v.
* PBRES (Push button reset):
This pin provides an active-low reset input to the engine board. It causes the
engine board to reset and start searching for satellites.
* SELECT :
Do not connect.
* 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
* RXA :
This is the main receive channel for receiving software commands to the engine
board from SiRFdemo software or from user written software.
Normally this pin must be kept in high, and if you don’t use this pin please
connect a resistor to pull high.
* Time mark :
This pin provides one pulse-per-second output from the engine board that is
synchronized to GPS time.
* GND :
GND provides the ground for the engine board. Connect all grounds.

SOFTWARE COMMAND
NMEA Output Command
GGA-Global Positioning System Fixed Data
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
Table B-2 GGA Data Format
Name
Example
Units
Description
Message ID
$GPGGA
GGA protocol header
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
HDOP
1.0
Horizontal Dilution of Precision
MSL Altitude
1
9.0
meters
Units
M
meters
Geoid Separation
1
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
SiRF Technology Inc. does not support geoid corrections. Values are WGS84 ellipsoid heights.
Table B-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 B-4 contains the values for the following example:
$GPGLL,3723.2475,N,12158.3416,W,161229.487,A*2C
Table B-4 GLL Data Format
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
GSA-GNSS DOP and Active Satellites
Table B-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 B-5 GSA Data Format
Name Example Units Description
Message ID $GPGSA GSA protocol header
Mode1 ASee Table B-6
Mode2 3See Table B-7
Satellite Used107 Sv on Channel 1
Satellite Used102 Sv on Channel 2
…..
Satellite Used1Sv 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
1. Satellite used in solution.
Table B-6 Mode1
Value Description
MManual-forced to operate in 2D or 3D mode
A2Dautomatic-allowed to automatically switch 2D/3D
Table B-7 Mode 2
Value Description
1 Fix Not Available
2 2D
3 3D

GSV-GNSS Satellites in View
Table B-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 B-8 GSV Data Format
Name
Example
Description
Message ID
$GPGSV
GSV protocol header
Number of Messages
1
2
Range 1 to 3
Message Number
1
1
Range 1 to 3
Satellites in View
07
Satellite ID
07
Channel 1(Range 1 to 32)
Elevation
79
degrees
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
Channel 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
Depending on the number of satellites tracked multiple messages of GSV data may be required.
RMC-Recommended Minimum Specific GNSS Data
Table B-10 contains the values for the following example:
$GPRMC,161229.487,A,3723.2475,N,12158.3416,W,0.13,309.62,120598,,*10
Table B-10 RMC Data Format
Name
Example
Units
Description
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
2
degrees
E=east or W=west
Checksum
*10
<CR><LF>
End of message termination
SiRF Technology Inc. does not support magnetic declination. All “course over ground” data are
geodetic WGS48 directions.

VTG-Course Over Ground and Ground Speed
$GPVTG,309.62,T,,M,0.13,N,0.2,K*6E
Name
Example
Units
Description
Message ID
$GPVTG
VTG protocol header
Course
309.62
degrees
Measured 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