Globalsat ER-332 User Manual Download Page 3

             

 

ER-332

                                                                                                       

 

Specifications are subject to be changed without notice. 

Page 3 of 14 

 

Version 1.3.1 

Reacquisition 0.1 

second 

average 

Accuracy 

Position: 10 meters, 2D RMS 
           5 meters, 2D RMS, WAAS enabled 
Velocity: 0.1 m/s   
Time: 1us synchronized to GPS time   

Maximum Altitude 

18,000 meter (60,000 feet) max 

Maximum Velocity 

515 meter/second (1000 knots) max 

Maximum Acceleration 

4G 

Jerk 

20m/sec **3

 

Interface 

I/O Connector Type 

 

External Antenna Port 

 

Physical Characteristic 

Dimensions 

1.6” x 1.4” x 0.4” (40.5 x 35 x 10 mm)   

DC Characteristics 

Power Supply 

3.8V ~ 6.5V DC Input 

Power Consumption 

42mA (Continuous Mode) 
25mA (Trickle Power Mode)

 

Environmental Range 

Humidity Range 

5% to 95% non-condensing 

Operation Temperature 

-40C to 85C   

Storage Temperature 

-40C to 85C 

   

 

 

Summary of Contents for ER-332

Page 1: ...332 Globalsat Technology Corporation 16F No 186 Jian Yi Road Chung Ho City Taipei Hsien 235 Taiwan Tel 886 2 8226 3799 Fax 886 2 8226 3899 service globalsat com tw www globalsat com tw USGlobalSat In...

Page 2: ...e NMEA 0183 data protocol 9 Foliage Lock for weak signal tracking 9 All in view 20 channel parallel processing 9 Snap Lock 100mc re acquisition time 9 Enhanced algorithm for navigation stability 9 Sup...

Page 3: ...ter 60 000 feet max Maximum Velocity 515 meter second 1000 knots max Maximum Acceleration 4G Jerk 20m sec 3 Interface I O Connector Type External Antenna Port Physical Characteristic Dimensions 1 6 x...

Page 4: ...ER 332 Specifications are subject to be changed without notice Page 4 of 14 Version 1 3 1 2 Technical Information Physical Characteristics...

Page 5: ...SELECT Reserved 11 TIMEMARK 1PPS Time Mark Output Output 12 GND Ground Pin Explanation VDC DC power input This is the main DC supply for a 3 8V 6 5V power module board VBAT Backup battery This is the...

Page 6: ...0 Ohm resistor in series with a 3 2v Zener diode to Ground Then connect the Rx input to Zener s cathode to pull the input HIGH Time mark This pin provides one pulse per second output from the engine b...

Page 7: ...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 dd...

Page 8: ...x 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...

Page 9: ...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 ddmmy...

Page 10: ...rotocol 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...

Page 11: ...tart 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 This command is used to control Serial Port B an...

Page 12: ...ecksum enabled PSRF103 05 00 01 01 20 Example 3 Disable VTG message PSRF103 05 00 00 01 21 E LLA Navigation initialization ID 104 Parameters required to start using Lat Lon Alt This command is used to...

Page 13: ...ed Invalid commands will generate debug information that should enable the user to determine the source of the command rejection Common input rejection problems are associated to invalid checksum or p...

Page 14: ...without notice Page 14 of 14 Version 1 3 1 Name Example Units Description Message ID PSRF106 PSRF106 protocol header Datum 178 21 WGS84 178 Tokyo_Mean 179 Tokyo_Japan 180 Tokyo_Korea 181 Tpkyo_Okinaw...

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