Anti-disturbance fault tolerant initial alignment for inertial navigation system subjected to multiple disturbances

Modeling error, stochastic error of inertial sensor, measurement noise and environmental disturbance affect the accuracy of an inertial navigation system (INS). In addition, some unpredictable factors, such as system fault, directly affect the reliability of INSs. This paper proposes a new anti-dist...

Full description

Bibliographic Details

Main Authors:	Songyin Cao, Lei Guo, Wen-Hua Chen
Format:	Default Article
Published:	2017
Subjects:	Aerospace engineering not elsewhere classified Mechanical engineering not elsewhere classified Other engineering not elsewhere classified Inertial navigation system Fault tolerant Filter Initial alignment Robustness Multiple disturbances Aerospace Engineering Mechanical Engineering Engineering not elsewhere classified
Online Access:	https://hdl.handle.net/2134/27526
Tags:	Add Tag No Tags, Be the first to tag this record!