Younis H. Karim, AbidYahya School of Computer University Malaysia Perlis 1.

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Younis H. Karim, AbidYahya School of Computer University Malaysia Perlis 1

Abstract With the growing use of the Global Positioning System (GPS) in many fields (air, land, sea and space) as advanced navigation system which provide high accurate and reliability for the position (latitude, longitude and altitude) and velocity with time. In this paper we tested the GPS system type Garmin-25LP to evaluate the accuracy of the system with different velocity and the angles of sight by integrated with a portable computer employing the National Marine Electronics Association (NMEA) software program. the changing of velocity by using private car and the effects of varying angles of sight of the GPS with satellites are investigated, the variation of the angles are achieved by means of using a specially designed blind regions platform. 2

Introduction Position and attitude parameters are important information in the navigation, control and guidance of moving platforms.GPS can consistently provide accurate position, velocity and timing information under good satellite signal tracking environments. The main factor limiting use of GPS is the requirement for line- of-sight between the receiver antenna and the satellites, which cannot always be met. Standard GPS position estimates can achieve accuracy on the order of meters to centimeters (Lachapelle, 2003), 3

 The Global Positioning System consists of three separate elements: the space segment, the control segment and the user segment. For the space segment, the GPS constellation consists of 24 satellites arrange in 6 orbital planes with 4 satellites per plane. GPS satellites transmit two codes: the Precision or P-code and the Coarse Acquisition or C/A code. 4

 The control segment tracks GPS satellite and provides them with periodic updates, correcting their ephemeris constant and clock- bias errors. The location of the stations is known with a high degree of accuracy and each station is equipped with a cesium atomic clock. Each satellite signals are read at least by four stations. Because the stations positions and time coordinates are known. The GPS user segment consists of GPS receivers and their auxiliary equipment such as antenna. 5

 GPS Garmin-25LP  The GARMIN GPS 25LP Series are GPS sensor boards designed for a broad spectrum of OEM (Original Equipment Manufacturer) system application. The GPS 25LP will simultaneously track up to twelve satellites providing fast time-to-first-fix, one second navigation updates and low power consumption. Their far-reaching capability meets the sensitivity requirements of land navigation as well as the dynamic requirements of high performance aircraft. 6

 The GPS 25LP is designed to withstand rugged operation conditions, however it should be mounted in an enclosure as part of a larger system designed by an OEM or system integrator. The system may communicate with the board set via a choice of two CMOS/TTL or two RS-232 compatible bi-directional communication channels. An on-board memory rechargeable backup battery allows the sensor board to retain critical data such as satellite orbital parameters, last position, date and time.  These data include: position (Latitude, Longitude, and Altitude), Velocity, Date/time, Error estimates and Satellite and Receiver status. 7

Figure (1) GPS 25 LP Block Diagram. 8

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10 Figure (2) change velocity with Latitude

11 Figure (3) change velocity with Longitude

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 Conclusion  In this study, the testing has been carried out using GPS Garmin 25LP.  From the both testing accuracy of velocity and testing of varying the angle of sight, we conclude that the GPS Garmin 25LP system is good accurate and reliability if used in vehicles or even in sailing boats. The system has good characteristics: single board integrated with complete component shielding, light weight, small size and separate antenna; however we recommend that the antenna of the system to be placed in good location Even be visible from the most many as possible of satellites. 16