Rikaline CF GPS Receiver Manual de usuario

【High Sensitivity】

CF GPS Receiver

May. 08, 2003

Rikaline International Corp.

10F, 64, Kang-Ding Road, Taipei 108, Taiwan, R.O.C.

Phone: +886-2-2370-4688 Fax: +886-2-2370-4686

E-Mail: [email protected] Web: www.rikaline.com.tw

User’s Guide

Rikaline GPS-6021-X6

High Sensitivity GPS-6021-X6 Operating Manual

Rikaline

Rikaline International Corp. 10F, 64, Kang-Ding Road, Taipei 108, Taiwan

Tel: ++886 2 2370 4688 Fax: ++886 2 2370 4686 E-Mail: [email protected]m.tw Web: www.rikaline.com.tw

TABLE OF CONTENTS

0. Quick USe ……….………………………………………………………………………………….. 3

0.1 Check GPS Package ..………………………………………………………………….. 3

0.2 Check Connector …..…………………………………………………………………….. 3

0.3 Connect GPS-6021-X6 to your machine ….………………………………………. 3

0.4 Turn on your machine …………………………………………………………………….. 3

0.5 Basic Specs …………………………………………………………………………………. 3

1. Introduction ……………………………………………………………………………………….. 4

1.1 Overview …………………………………………………………………………………….. 4

1.2 Features …………………………………………………………………………………….. 4

1.3 Technical Specifications ……………………………………………………………….. 4

2. Operational Characteristics ……………………………………………………………….… 6

2.1 Initialization …………………………………………………………………………………. 6

2.2 Navigation …………………………………………………………………………………. 6

3. Hardware Interface ………………………………………………………………………….…… 7

3.1 Dimension ………………………………………………………………………………….… 7

3.2 Hardware Interface

…..……………………………………………………………….…… 7

3.3 Connector ………………………………………………………………………………….… 7

3.4 Accessories …………………………………………………………………………………. 8

4. PCMCIA Installation File …………………………………………………………………….… 8

4.1 System Requirement

……………………………………………………………………… 8

4.2 Installation ………………….…………………………………………………………….… 8

5. Waranty …………………………………………………………………………………………….… 8

Appendix A Software Inferface ……………………………………………………………. 9

A.1 NMEA Transmitted Sentences ……………………………………………………..… 9

A.2 RTCM Received Data ………………………………………………………………….. 12

Appendix B Earth Datums and Output Setting ……………………………………… 13

B.1 Earth Datums ………..…………………………………………………………………….. 13

B.2 Setting ……..……………………………………………………………………………….… 13

Appendix C Products Information ……………………………………………………….. 14

C.1 Product Options ……………………………………………………………….………… 14

C.2 Optional Accessories …………………………………………………………….……… 14

High Sensitivity GPS-6021-X6 Operating Manual

Rikaline

Rikaline International Corp. 10F, 64, Kang-Ding Road, Taipei 108, Taiwan

Tel: ++886 2 2370 4688 Fax: ++886 2 2370 4686 E-Mail: [email protected]m.tw Web: www.rikaline.com.tw

0. Quick Use

0.1 Check GPS Package

0.1.1 Standard Package

GPS-6021-X6 (GPS Receiver) + CD + Warranty Card + quick installation reference.

0.1.2 Optional Package

The shop may bundle different accessories for you as follows:

1. Active Antenna

2. PCMCIA Adapter

3. PDAHolder

4. Software (Navigation Software + Digital Map)

5. Others

0.2 Check CF Card Slot

1. The GPS-6021-X6 is a Type I CF device. Many new PDAs are equipped with Type II CF slot. Make

sure to slot in properly to avoid damage.

2. When you connect GPS-6021-X6 with your PC (Webpad PC, Tablet PC, Laptop PC or other PCs) with

PCMCIA adapter, you need to point to an installation file included in the CD.

0.3 Connect GPS-6021-X6 to your machine.

0.4 Turn on your machine & Start GPS function.

You may need to execute navigation software, then link to GPS device. YOur GPS-6021-X6 starts to

provide you full GPS function.

0.5 Basic Specifications

1. CF type I: Suitable to CF Type I and Type II slot.

High Sensitivity GPS-6021-X6 Operating Manual

Rikaline

Rikaline International Corp. 10F, 64, Kang-Ding Road, Taipei 108, Taiwan

Tel: ++886 2 2370 4688 Fax: ++886 2 2370 4686 E-Mail: [email protected]m.tw Web: www.rikaline.com.tw

1. Introduction

1.1 Overview

The Rikaline GPS-6021-X6 High Sensitivity CF GPS Receiver is a total solution GPS receiver, designed

based on SiRF Star II Architecture with the newest high sensitivity system. This revolutionary system

provides you unbelievable positioning sensitivity allowing you to have easy position fix in urban canyon

conditions. This positioning application meets strict needs such as car navigation, mapping, surveying, security,

agriculture and so on. Only clear view of sky and certain power supply are necessary to the unit. It

communicates with other electronic utilities via compatible dual-channel through RS-232 and saves critical

satellite data by built–in backup memory. With low power consumption, the GPS-6021-X6 tracks up to 12

satellites at a time, re-acquires satellite signals in 100 ms and updates position data every second.

Trickle-Power allows the unit operates a fraction of the time and Push-to-Fix permits user to have a quick

position fix even though the receiver usually stays off.

1.2 Features

The GPS-6021-X6 provides a host of features that make it easy for integration and use.

1. SiRF Star II chipset with embedded ARM7TDMI CPU available for customized applications in firmware.

2. High performance receiver tracks up to 12 satellites while providing first fast fix and low power

consumption.

3. Differential capability utilizes real-time RTCM corrections producing 1-5 meter position accuracy.

4. Compact design ideal for applications with minimal space.

5. A rechargeable battery sustains internal clock and memory. It is recharged during normal operation.

6. User initialization is not required.

7. Dual communication channels and user selectable baud rates allow maximum interface capability and

flexibility.

8. FLASH based program memory: New software revisions upgradeable through serial interface.

9. LED display status: The LED will be “ON” when power connected.

10. Built-in WAAS / EGNOS demodulator.

11. Small size.

1.3 Technology specifications

1.3.1 Physical Dimension

Single construction integrated antenna/receiver.

Size: 83.0(H) x 47.5(W) x 14.5(D) (mm)

3.27"(H) x 1.87"(W) x 0.57"(D).

1.3.2 Environmental Characteristics

1) Operating temperature: -40oC to +85oC(internal temperature).

2) Storage temperature: -55oC to +100oC.

1.3.3 Electrical Characteristics

1) Input voltage: +2.5 ~ 5.5 VDC without accessories.

2) Backup power: 3V Rechargeable Lithium cell battery, up to 767 hours (31.9 days) discharge.

1.3.4 Performance

1) Tracks up to 12 satellites.

2) Update rate: 1 second.

3) Acquisition time

Reacquisition 0.1 sec., averaged

Snap start 2 sec., averaged

Hot start 8 sec., averaged

Warm start 38 sec., averaged

High Sensitivity GPS-6021-X6 Operating Manual

Rikaline

Rikaline International Corp. 10F, 64, Kang-Ding Road, Taipei 108, Taiwan

Tel: ++886 2 2370 4688 Fax: ++886 2 2370 4686 E-Mail: [email protected]m.tw Web: www.rikaline.com.tw

Cold start 45 sec., averaged

4) Position Accuracy

A) Non DGPS (Differential GPS)

Position 15-meter 2D RMS

7-meter 2D RMS with WAAS corrected

Velocity 0.1 meters/second, with SA off

Time 1 microsecond synchronized GPS time

B) DGPS (Differential GPS)

Position 1 to 5 meter, typical

Velocity 0.05 meters/second, typical

5) Dynamic Conditions:

Altitude 18,000 meters (60,000 feet) max

Velocity 515 meters / second (1000 knots) max

Acceleration 4 G, max

Jerk 20 meters/second3

, max

1.3.5 Interfaces

1) Dual channel RS-232 level, with user selectable baud rate (4800-Default, 9600, 19200, 38400).

2) NMEA 0183 Version 2.2 ASCII output (GPGGA, GPGLL, GPGSA, GPGSV, GPRMC, GPVTG).

3) Real-time Differential Correction input (RTCM SC-104 message types 1, 5 and 9).

4) SiRF protocol.

High Sensitivity GPS-6021-X6 Operating Manual

Rikaline

Rikaline International Corp. 10F, 64, Kang-Ding Road, Taipei 108, Taiwan

Tel: ++886 2 2370 4688 Fax: ++886 2 2370 4686 E-Mail: [email protected]m.tw Web: www.rikaline.com.tw

2. Operational characteristics

2.1 Initialization

As soon as the initial self-test is complete, the GPS-6021-X6 begins the process of satellite acquisition and

tracking automatically. Under normal circumstances, it takes approximately 45 seconds to achieve a position fix,

38 seconds if ephemeris data is known. After a position fix has been calculated, information about valid position,

velocity and time is transmitted over the output channel.

The GPS-6021-X6 utilizes initial data, such as last stored position, date, time and satellite orbital data, to

achieve maximum acquisition performance. If significant inaccuracy exists in the initial data, or the orbital data

is obsolete, it may take more time to achieve a navigation solution. The GPS-6021-X6 Auto-locate feature is

capable of automatically determining a navigation solution without intervention from the host system. However,

acquisition performance can be improved when the host system initializes the GPS-6021-X6 in the following

situation:

1) Moving further than 1,500 kilometers.

2) Failure of data storage due to the inactive internal memory battery.

2.2 Navigation

After the acquisition process is complete, the GPS-6021-X6 sends valid navigation information over output

channels. These data include:

1) Latitude/longitude/altitude

2) Velocity

3) Date/time

4) Error estimates

5) Satellite and receiver status

The GPS-6021-X6 sets the default of auto-searching for real-time differential corrections in RTCM SC-104

standard format, with the message types 1, 5, or 9. It accomplishes the satellite data to generate a differential

(DGPS) solution. The host system, at its option, may also command the GPS-6021-X6 to output a position

whenever a differential solution is available.

High Sensitivity GPS-6021-X6 Operating Manual

Rikaline

Rikaline International Corp. 10F, 64, Kang-Ding Road, Taipei 108, Taiwan

Tel: ++886 2 2370 4688 Fax: ++886 2 2370 4686 E-Mail: [email protected]m.tw Web: www.rikaline.com.tw

3. Hardware interface

3.1 Dimension

Size: 83.0(H) x 47.5(W) x 14.5(D) (mm)

3.27"(H) x 1.87"(W) x 0.57"(D).

3.2 Hardware Interface

The GPS-6021-X6 includes an antenna in a unique style gadget. Simply put it into a CF card slot or

insert it into PCMCIA slot through a PCMCIA adapter of any type of PC with Windows OS. The interface is

through a standard 50-pin PCMCIA connector with RS-232 level.

.3 Connector

1) Standard 50-pin CF female connector.

2) Optional active antenna female connector.

3.3.1 Function definition of CF card connector

Please download detail at http://compactflash.org/specdl1.htm

3.4 Accessories

3.4.1 Active Antenna

A-10302-M Active Antenna with 2 meter 180°MMCX connector

A-10305-M Active Antenna with 5 meter 180°MMCX connector

High Sensitivity GPS-6021-X6 Operating Manual

Rikaline

Rikaline International Corp. 10F, 64, Kang-Ding Road, Taipei 108, Taiwan

Tel: ++886 2 2370 4688 Fax: ++886 2 2370 4686 E-Mail: [email protected]m.tw Web: www.rikaline.com.tw

4. PCMCA Installation File

4.1 System Requirements

IBM, Pentium or other compatible PC, Windows 98/Me/2000.

4.2 Installation

1. Turn your PC.

2. Your PC will show new device found.

3. Indicate to the direction you store GPS-6021-X6.inf file.

4. Click “Yes”. Your PC will installation the file automatically.

Note: 1// The GPS-6021-X6.inf installation file is needed when a PCMCIA adapter used.

2// PDA does not need to install any extra file.

5. Warranty

The GPS-6021-X6 is warranted to be free from defects in material and functions for one year from the

date of purchase. Any failure of this product within this period under normal conditions will be replaced at no

charge to the customers.

High Sensitivity GPS-6021-X6 Operating Manual

Rikaline

Rikaline International Corp. 10F, 64, Kang-Ding Road, Taipei 108, Taiwan

Tel: ++886 2 2370 4688 Fax: ++886 2 2370 4686 E-Mail: [email protected]m.tw Web: www.rikaline.com.tw

Appendix A Software Interface

The GPS-6021-X6 interface protocol is based on the National Marine Electronics Association's NMEA

0183 ASCⅡinterface specification, which is defined in NMEA 0183, Version 2.2 and the Radio Technical

Commission for Maritime Services (RTCM Recommended Standards For Differential Navstar GPS Service,

Version 2.1, RTCM Special Committee No.104).

A.1 NMEA Transmitted Messages

The GPS-6021-X6 supported by SiRF Technology Inc. also outputs data in NMEA-0183 format as defined

by the National Marine Electronics Association (NMEA), Standard.

The default communication parameters for NMEA output are 4800 baud, 8 data bits, stop bit, and no parity.

Table A-1 NMEA-0183 Output Messages

NMEA Sentence Description

GPGGA Global positioning system fixed data

GPGLL Geographic position latitude \ longitude

GPGSA GNSS DOP and active satellites

GPGSV GNSS satellites in view.

GPRMC Recommended minimum specific GNSS data

GPVTG Coruse over ground and ground speed

A.1.1 Global Positioning System Fix Data (GGA)

Table A-2 contains the values for the following example:

$GPGGA,161229.487,3723.2475,N,12158.3416,W,1,07,1.0,9.0,M, , , ,0000*18

Table A-2 GGA Data Format

Name Example Units Description

Message ID $GPGGA GGA protocol header

UTC Time 161229.487 Hhmmss.sss

Latitude 3723.2475 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

Position Fix Indicator 1 See Table 5-3

Satellites Used 07 Range 0 to 12

HDOP 1.0 Horizontal Dilution of Precision

MSL Altitude 9.0 Meters

Units M Meters

Geoid Separation Meters

Units M Meters

Age of Diff. Corr. second Null fields when DGPS is not used

Diff. Ref. Station ID 0000

Checksum *18

<CR> <LF> End of message termination

Table A-3 Position Fix Indicator

Value Description

0 0 Fix not available or invalid

1 GPS SPS Mode, fix valid

2 Differential GPS, SPS Mode, fix valid

3 GPS PPS Mode, fix valid

High Sensitivity GPS-6021-X6 Operating Manual

Rikaline

Rikaline International Corp. 10F, 64, Kang-Ding Road, Taipei 108, Taiwan

Tel: ++886 2 2370 4688 Fax: ++886 2 2370 4686 E-Mail: [email protected]m.tw Web: www.rikaline.com.tw

A.1.2 Geographic Position with Latitude/Longitude (GLL)

Table A-4 contains the values for the following example:

$GPGLL,3723.2475,N,12158.3416,W,161229.487,A*2C

Table A-4 GLL Data Format

Name Example Units Description

Message ID $GPGLL GLL protocol header

Latitude 3723.2475 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

UTC Position 161229.487 hhmmss.sss

Status A A=data valid or V=data not valid

Checksum *2C

<CR> <LF> End of message termination

A.1.3 GNSS DOP and Active Satellites (GSA)

Table A-5 contains the values for the following example:

$GPGSA,A,3,07,02,26,27,09,04,15, , , , , ,1.8,1.0,1.5*33

Table A-5 GSA Data Format

Name Example Units Description

Message ID $GPGSA GSA protocol header

Mode 1 A See Table 5-6

Mode 2 3 See Table 5-7

Satellite Used (1) 07 Sv on Channel 1

Satellite Used (1) 02 Sv on Channel 2

…… ….

Satellite Used Sv on Channel 12

PDOP 1.8 Position Dilution of Precision

HDOP 1.0 Horizontal Dilution of Precision

VDOP 1.5 Vertical Dilution of Precision

Checksum *33

<CR> <LF> End of message termination

(1) Satellite used in solution.

Table A-6 Mode 1

Value Description

M Manual—forced to operate in 2D or 3D mode

A2D Automatic—allowed to automatically switch 2D/3D

Table A-7 Mode 2

Value Description

1 Fix Not Available

2 2D

3 3D

A.1.4 GNSS Satellites in View (GSV)

Table A-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,2,2,07,09,23,313,42,04,19,159,41,15,12,041,42*41

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