Title: SINS/CNS/GPS Combined navigation semi-entity copying system
Application Number: 200610011580 Application Date: 2006.03.29
Publication Number: 1834980 Publication Date: 2006.09.20
Approval Pub. Date: Granted Pub. Date:
International Classifi-cation: G06G7/78
Applicant(s) Name: Beijing Aeronautics Address: 100083
Inventor(s) Name: Fang Jiancheng, Xu Fan, Quan Wei, Sheng Yu, Liu Ba
Attorney & Agent: liu xiujuan cheng jinyu
Abstract:
     The invention is a SINS/CNS/GPS combined-navigating half-entity simulating system, comprising SINS, CNS and GPS subsystems, combined navigating computer and track generator, using SINS and GPS entity systems, star map simulator and star sensor simulator entity as physical models, combined navigating computer, where the combined navigating computer adopts PC104 embedded microcomputer, the track generator software produces nominal track data, and dynamic characteristics of the system adopt digital model and it performs SINS/CNS/GPS combined navigating operation in the combined navigating computer to complete SINS/CNS/GPS combined navigation. And it effectively reduces testing cost and shortens development cycle.
Time: 11
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