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

3.0 Technical configuration

This section provides a detailed description of all the technical aspects and configurable 

functionality of the Jupiter 20 GPS Development Unit.

3.1 Overview

Figure 3-1 illustrates the connectors, switches and LEDs available on the Development Unit.

1   2   3   4   5   6   7   8

CTS     206-8     T114

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power switch

configuration switch

function LEDs

reset switch

Serial Port 1

Antenna

DR

Clock

Out

Serial Port 2

-

+

DC Power

9-16Volts

1PPS output

comm 1 

NMEA & binary

comm 2 

(RTCM)

dead reckoning

 

input signals

DC input J1

‘U’ slot for antenna

 

cable (custom)

SMA antenna

 

connector

Figure 3-1 Front and back panels of the Jupiter 20 development unit

3.1.1 Power switch (ON/OFF)

The switch on the front panel controls primary power to the Jupiter 20 receiver module inside. 

The power status LED (see section 3.3) indicates status: if lit, the module has primary power 

supplied. If the configuration DIP switch 5 is on and Jumper JB5/6 linked, the module’s 

secondary supply SRAM and RTC will continue to be powered when the power switch is off. 

Only removal of the DC power input at the rear 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’ capability when primary power is 

re-applied within 4 hours, and a ‘warm start’ thereafter, by maintaining last position, current time 

and satellite ephemerides.

3.1.2 Configuration DIP switch

The configuration DIP switch on the front panel provides the ability to configure the Jupiter 

20 module, offering flexibility depending on the specific application. Refer to section 3.2 for 

a description of the functionality of each individual switch, including the typical settings when 

using the Jupiter 20 module.

3.1.3 Function LEDs

The four LEDs on the front panel indicate the current status of basic features associated with 

the Development Unit. Refer to section 3.3 for a description of the function of each LED. 

3.1.4 Reset switch

A reset push button is provided on the front panel to generate a receiver system hardware reset. 

3.1.5 Clock out connector

The Clock out connector, located on the rear panel of the Development Unit, can be used to 

provide module generated timing signals. Refer to section 3.4 for more detailed information.

3.1.6 Serial port 1

This host serial port is used to send and receive serial data. This port is used as the default, with 

transmission in NMEA format at the rate of 9600 Baud. Use 9-pin D-subminiature connectors 

with these serial ports.

Содержание LA000507

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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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