background image

J5

+3.3 VDC,

 

or +5 VDC

direction 

F/R

reserved

wheel

 

ticks

1

2

3

4

5

6

gyro

ground

Figure 5-1 DR interface connector (rear of unit)

5.1.1 Pin 1 – DC power supply

This pin can be used to power at either 3.3 or 5 VDC for external devices used in the DR 

operation. To modify the supply voltage, refer to section 3.5 for details of the jumper positioning. 

5.1.2 Pin 2 – Heading rate gyro input

Table 5-1 details the gyro requirements. It is important to ensure that the rate gyro signals have 

the following characteristics:

• Range: 0 to 5 V
• Output (no gyro rotation): 2.5 V
• Clockwise rotation of the gyro causes the output voltage to rise
• Maximum voltage deviation due to rotation should occur with a turning rate of 90º per 

second or less

14

LA000510C © 2006 Navman NZ Ltd. All rights reserved. Proprietary information and specifications subject to change without notice.

To set the receiver output to SiRF binary

1. Open the SiRFDemo software.
2. When the Data Source setup is displayed, select the appropriate COM port and 9600 Baud 

from the drop down menu.

3. Select the Action menu and click on Open Data Source. If the Development Unit is powered, 

and the serial port is connected to the PC, NMEA data should appear in the Debug View 

window. 

To change to SiRF binary, select the Action menu and click on the Switch to SiRF Protocol. This 

should now present information in each window, similar to that of VisualGPS. Whilst enabled in 

SiRF binary protocol, more of the analysis software’s functionality can be accessed. To switch 

back into NMEA mode, select the Action menu and click on Switch to NMEA Protocol. Select 

9600 for the baud rate and click on the Send button.

Note:

 settings, including the current output protocol, are reset if all power is removed from the 

unit. For more information, refer to the SiRFDemo and SiRFFlash User Guides.

5.0 Jupiter 20 DR (Dead Reckoning) configuration

The DR connector on the rear panel of the Development Unit provides an interface with the 

external inputs under DR operation. This functionality is only to be used when evaluating Jupiter 

20 DR modules.

The connector is used for signals transmitted by:

• An angular rate sensor (gyro)
• A wheel ticks source
• A forward/reverse indicator

These signals are present on many late model vehicles and may be used to assist the DR 

receiver in determining position accuracy during the loss of signal conditions. Direct connection 

to the vehicle is not normally possible as the inputs need to be 3 V logic level signals.

Note:

 when using the Jupiter 20 DR version in a Development Unit, the front panel switches 1, 

2, 3 and 4 should be isolated by turning the internal switches SW3 OFF. If the front panel 
DIP switch 3 is still required, leave the internal switch SW3.3 ON.

5.1 DR connector pin configuration

The following sections describe the functions of the DR connector pins. Refer to Figure 5-1.

Summary of Contents for LA000507

Page 1: ...dead reckoning TU20 D421 201 Related documents Jupiter 20 Product brief LA000509 Jupiter 20 Data sheet LA000507 Jupiter 20 DR Application note LA000433 Jupiter 30 20 Integrator s manual LA000577 SiRF...

Page 2: ...DIP switch 6 Antenna preamp power select 3 3 V or 5 12 V 8 3 2 7 DIP switch 7 Antenna preamp power select 5 V or 12 V 8 3 2 8 DIP switch 8 Antenna preamp power enable 8 3 3 Function LEDs 8 3 3 1 1PPS...

Page 3: ...4 Pin layout of the clock out connector 9 Figure 3 5 Internal layout of the Development Unit 9 Figure 3 6 Jupiter 20 adapter board 11 Figure 4 1 Development Unit test equipment 13 Figure 5 1 DR interf...

Page 4: ...rce for SRAM and RTC Provision to insert a current measuring device to monitor both primary and backup power usage under various conditions Regulated DC power supply to the Jupiter 20 module Status in...

Page 5: ...alysis software are also provided to allow communication with the Jupiter 20 GPS receiver through a serial port This Windows based software presents the receiver s raw data in a geographical form allo...

Page 6: ...r of the unit will stop secondary power being applied assuming Jumper JB5 6 and switch 5 are correctly set Having this secondary power supply applied means that the Jupiter 20 will have a hot start ca...

Page 7: ...FR OFF high 3 Serial BOOT OFF normal run 4 GPIO1 W_TICKS OFF high 5 RTC BACKUP POWER ON enabled 6 PREAMP power select OFF 3 V 7 PREAMP power select OFF 12 V 8 PREAMP power enable ON enabled These fun...

Page 8: ...s of switches 7 and 8 also need to be considered when using the preamp function Note the supplied antenna is a 3 3 V type 3 2 7 DIP switch 7 Antenna preamp power select 5 V or 12 V DIP switch 7 also c...

Page 9: ...round Table 3 2 Pin functions of the clock out connector 4 3 2 1 Figure 3 4 Pin layout of the clock out connector A mating connector for the clock out connector is supplied with the Development kit Th...

Page 10: ...3 3 V supplied to Pin 1 of the DR connector JB13 14 not used JB14 15 not used JB16 17 Internal interface enable normally fitted Table 3 4 Pin functionality In addition to the configurable jumpers the...

Page 11: ...e connectors and indicators Figure 3 6 Jupiter 20 adapter board Table 3 6 lists the pin configurations for the J1 and J2 connectors Jupiter function J2 2 54 mm pitch header pin no J1 2 mm pitch header...

Page 12: ...a clear view of the sky for optimal reception of the satellite signals The 1PPS LED should begin flashing at 1 Hz once the receiver is powered and has started receiving at least one satellite This pro...

Page 13: ...ualGPS VisualGPS graphically presents the serial data transmitted by the receiver The receiver output must be enabled in the NMEA protocol for this software to be used To enable the receiver output 1...

Page 14: ...d now present information in each window similar to that of VisualGPS Whilst enabled in SiRF binary protocol more of the analysis software s functionality can be accessed To switch back into NMEA mode...

Page 15: ...normally at 0 V but rises to 3 V when the vehicle is in the reverse gear Use of this signal is optional if it is not used the effect of occasional reversing by the vehicle will not significantly degr...

Page 16: ...DUCTS INCLUDING LIABILITY OR WARRANTIES RELATING TO FITNESS FOR A PARTICULAR PURPOSE CONSEQUENTIAL OR INCIDENTAL DAMAGES MERCHANTABILITY OR INFRINGEMENT OF ANY PATENT COPYRIGHT OR OTHER INTELLECTUAL P...

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