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

3.1.7 Serial port 2

This is the auxiliary serial port, primarily used for the reception of RTCM SC-104 DGPS 

(Differential GPS) correction messages.

3.1.8 DR connector

The DR connector is used to interface with a gyroscope, wheel tick pulses and forward/reverse 

indicator when using a Jupiter 20 DR module. Refer to section 3.5 for more information.

3.1.9 Antenna connector

The antenna provided with this Development kit should be connected to the SMA connector 

located on the rear panel of the Development Unit.

3.1.10 DC power input

The supplied DC power adapter should be plugged into the DC connector on the rear panel of 

Development Unit. The Development Unit will accept voltages from 9 to 16 VDC. The middle pin 

on J1 is negative polarity, while the outer shell is positive.

3.2 Configuration DIP switch

A typical setting of the Configuration DIP switch is shown in Figure 3-2.

 

ON

OFF

1   2   3   4    5   6   7   8

Figure 3-2 Configuration DIP switch

Table 3-1 outlines the available functionality and corresponding switch position for the 

Configuration DIP switch.

Switch

Description

Typical setting

1

GPIO3/GYROIN*

OFF (high)

2

GPIO15/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 functions have been disabled by internal switch SW3 to allow correct operation of 

the antenna current sense circuits on the Jupiter 20 adapter board.

Table 3-1 DIP switch settings

A brief description of the functionality of each switch is specified below. Refer to the Jupiter 20 

Data sheet for more information about the functionality of specific pads. The receiver 

operating settings will not change after moving the position of a configuration switch while the 

Development Unit is operating. Pressing the reset switch, or turning the unit OFF and ON will 

enable the settings to take effect in the receiver. The recommended method for reconfiguration 

is to switch the unit OFF, modify the switch positions, then re-apply the power.

3.2.1 DIP switch 1 – GPIO3 /GYROIN input

DIP switch 1 interfaces with the GPIO3 /GYROIN pad of the module. The switch is typically 

OFF, but has no effect with the standard module’s software. This switch can be enabled by the 

internal switch SW3.1.

3.2.2 DIP switch 2 – GPIO15 /FR input

DIP switch 2 interfaces with the GPIO15 /FR pad of the module. The switch is typically OFF, but 

has no effect with the standard module’s software. This switch can be enabled by the internal 

switch SW3.2.

3.2.3 DIP switch 3 – BOOT from serial mode

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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