DocumentCode :
3532509
Title :
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
Link To Document :
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