Navman LA000507 - Manuals

Navman LA000507 – Manual in PDF format online.

Manuals:

Manual

Manual Navman LA000507

Summary

Page 2 - Technical configuration

LA000510C © 2006 Navman NZ Ltd. All rights reserved. Proprietary information and specifications subject to change without notice . Contents1.0 Introduction ....................................................................................................... 42.0 Equipment.............................

Page 4 - Equipment supplied; This kit should contain the items illustrated in Figure 2-1.; Jupiter 20 GPS Development Unit; usage under various conditions; Serial interface cable

(1) (2) (3) (4) (5) (6) software and documentation Serial Port 1 Antenna DR Clock Out Serial Port 2 - + DC Power 9-16Volts 4 LA000510C © 2006 Navman NZ Ltd. All rights reserved. Proprietary information and specifications subject to change without notice. 1.0 Introduction The TU10-D007-400 series of ...

Page 5 - and evaluation for both NMEA and SiRF Binary formats.; Equipment required

5 LA000510C © 2006 Navman NZ Ltd. All rights reserved. Proprietary information and specifications subject to change without notice. 5. Power adapter for 12 VDC vehicle operation For mobile operation, an automotive adapter intended for use in 12 VDC vehicles is provided. 6. Software and documentation...

Page 6 - functionality of the Jupiter 20 GPS Development Unit.; Figure 3-1 Front and back panels of the Jupiter 20 development unit; and satellite ephemerides.; with these serial ports.

6 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 U...

Page 7 - Configuration DIP switch; ON; Configuration DIP switch.; Switch; Serial BOOT; Table 3-1 DIP switch settings

7 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 T...

Page 8 - DIP switch 5 – RTC backup power enable; even with the main power switch in the OFFposition.; DIP switch 8 – Antenna preamp power enable; the active antenna supplied with the kit.; Figure 3-3 Function LEDs on front panel; This LED indicates presence of primary DC power to the module.

8 LA000510C © 2006 Navman NZ Ltd. All rights reserved. Proprietary information and specifications subject to change without notice. DIP switch 3 interfaces with the BOOT pad of the module and allows the user to upgrade the Flash memory. For normal operation the switch should be set to OFF. To boot f...

Page 9 - Clock out connector; Pin number; not used; Table 3-2 Pin functions of the clock out connector; Manufacturer; Molex; Table 3-3 Mating connector part description; Internal configuration; illustrates the internal layout of the Development Unit board.; Figure 3-5 Internal layout of the Development Unit

ON/OFF switch configuration DIP switch function LEDS JB5/6 reset switch serial port 1 serial port 2 timing connector DR connector DC power JB10/11/12 voltage selection switch (3.3V or 5V) JB1/2 JB3/4 JB13/14/15 test points E1 to E9 JB16/17 SW3 all off except SW3.3 9 LA000510C © 2006 Navman NZ Ltd. A...

Page 10 - Table 3-4 Pin functionality; signals available on the test points are shown in Table 3-5.; Test point; Table 3-5 Signals available on the test points; in conjunction with the Development Unit. These are as follows:

10 LA000510C © 2006 Navman NZ Ltd. All rights reserved. Proprietary information and specifications subject to change without notice. Pins Function when linked JB1/2 Current link for 5 V supply. Can be used to determine current on 5 V rail. Not used for the Jupiter 20 module. JB3/4 Current link for t...

Page 11 - Jupiter 20 module on adapter board; Figure 3-6 Jupiter 20 adapter board; Table 3-6 lists the pin configurations for the J1 and J2 connectors.; Jupiter function; GND

Jupiter 20 module antenna power LED GPS fix LED J1 J2 (not normally fitted) RTC backup battery (not normally fitted) 11 LA000510C © 2006 Navman NZ Ltd. All rights reserved. Proprietary information and specifications subject to change without notice. 3.6 Jupiter 20 module on adapter board Figure 3-6 ...

Page 12 - Operating instructions; Initial connection and operation; Development Unit’s Serial Port 1.; Positioning the GPS antenna

12 LA000510C © 2006 Navman NZ Ltd. All rights reserved. Proprietary information and specifications subject to change without notice. 4.0 Operating instructions This section provides important information for the evaluation of the Jupiter 20 GPS module. Step-by-step instructions for connecting and op...

Page 13 - Figure 4-1 Development Unit test equipment; Operating the GPS Analyser software; must be enabled in the NMEA protocol for this software to be used.; To enable the receiver output; the Baud rate to 9600 Baud.

13 LA000510C © 2006 Navman NZ Ltd. All rights reserved. Proprietary information and specifications subject to change without notice. Figure 4-1 Development Unit test equipment The Development Unit should be set up as shown in Figure 4-1 with only the RTCM correction source connected to the receiver....

Page 14 - the following characteristics:; To set the receiver output to SiRF binary; from the drop down menu.; DR connector pin configuration

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 ...

Page 15 - factor; Table 5-1 Gyro input specifications; Acronyms used in this document; National Marine Electronics Association

15 LA000510C © 2006 Navman NZ Ltd. All rights reserved. Proprietary information and specifications subject to change without notice. The gyro should be mounted so that its sensitive axis is as near vertical as practical. Deviations from the vertical will reduce sensitivity for heading changes in the...