Development of a Test System of SINS/GPS Integrated Navigation System

Author

Guang-Jun He ; Bao-Quan Li ; Jiu-Yang Wang ; Jin-Bo Wang

Author_Institution

Coll. of Missile, Air force Eng. Univ., Sanyuan

fYear

2009

fDate

28-29 April 2009

Firstpage

1

Lastpage

4

Abstract

A real time network is introduced to the development of a test system of SINS/GPS (ship´s inertial navigation system/Global Position System) integrated navigation system. Because only the three-axis angular motions can but the three-axis linear motions can´t be emulated by three-axis revolving table, the complete navigation computing is accomplished by external compensation of linear motions. A navigation computer featured with close-coupled master-slave dual processors is developed, which can work fluently and rapidly, and can meet the requirements for the integrated navigation system on navigation computer I/O, data processing capability, size, weight, power consumption, etc.

Keywords

Global Positioning System; aerospace computing; inertial navigation; SINS-GPS integrated navigation system; close-coupled master-slave dual processors; navigation computer; ship inertial navigation system-Global Position System; test system; three-axis angular motions; three-axis linear motions; Communication system control; Computational modeling; Computer displays; Computer networks; Computer simulation; Global Positioning System; Inertial navigation; Missiles; Silicon compounds; System testing;

fLanguage

English

Publisher

ieee

Conference_Titel

Testing and Diagnosis, 2009. ICTD 2009. IEEE Circuits and Systems International Conference on

Conference_Location

Chengdu

Print_ISBN

978-1-4244-2587-7

Type

conf

DOI

10.1109/CAS-ICTD.2009.4960807

Filename

4960807