A detection system for field comprehensive performance of airborne model laser inertial navigation

• Main Authors: WANG LEI, KONG DEYING, ZHANG ZHENGYONG, LIU JIAN, LIU YONGJIAN, HU XIAOXING, WU ZHENGUO, CHEN SHANQIU, ZHANG LIN
• Format: Patent
• Language: English
• Published: 13.05.2015
• Subjects: GYROSCOPIC INSTRUMENTS; MEASURING; MEASURING DISTANCES, LEVELS OR BEARINGS; NAVIGATION; PHOTOGRAMMETRY OR VIDEOGRAMMETRY; PHYSICS; SURVEYING; TESTING

A detection system for field comprehensive performance of airborne model laser inertial navigation is disclosed. The detection system organically combines an intelligent testing system and a test vehicle, facilitates laser inertial navigation function testing and performance and precision verification in the field, and achieves rapid fault positioning and war preparation guarantee requirements of laser inertial navigation. The test vehicle is a carrier tool and the main structure of the whole testing system, can stimulate inertial navigation dynamic working environments, and can rapidly send testing equipment to the field to perform function performance detection and fault maintenance. The intelligent testing system comprises a vehicle-mounted power source system and a vehicle-mounted measurement and control system, and achieves function, performance and simulation testing and a fault detection function. The detection system can stimulate the inertial navigation dynamic working environments to performance various performance tests, can achieve precision verification combining static stimulated flight and dynamic vehicle mounting, facilitates function performance testing and fault detection and maintenance of the inertial navigation in the field, and achieves intelligent fault positioning of the laser inertial navigation and automatic function performance verification.