Fault diagnosis method and system for airborne inertial navigation system

The invention discloses a fault diagnosis method and a fault diagnosis system for an airborne inertial navigation system, which are characterized in that a composition structure of the inertial navigation system is determined by deeply analyzing a fault mode and influence of the airborne inertial na...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	WANG LIZHI, LI SHIXIANG, REN ZIKUN, XU YONG
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	GYROSCOPIC INSTRUMENTS MEASURING MEASURING DISTANCES, LEVELS OR BEARINGS NAVIGATION PHOTOGRAMMETRY OR VIDEOGRAMMETRY PHYSICS SURVEYING TESTING
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