Navigation Switching Strategy-Based SINS/GPS/ADS/DVL Fault-Tolerant Integrated Navigation System

被引:3
|
作者
Li W. [1 ]
Zhang R. [1 ]
Lei H. [2 ]
机构
[1] Northwestern Polytechnical University, Xi'an
[2] AVIC xi'An Flight Automatic Control Research Institute, Xi'an
关键词
Compendex;
D O I
10.1155/2021/9943370
中图分类号
学科分类号
摘要
Considering the conventional federated filtering-based fault-Tolerant integrated navigation system is difficult to be implemented by serial data processing circuits, this paper presents navigation switching strategy-based SINS/GPS/ADS/DVL fault-Tolerant integrated navigation system to guarantee the reliability of integrated navigation system under sensor faults. When sensor failure appears, SINS and fault-free sensors are selected successively to form an integrated navigation system, such that reliable navigation parameters can be obtained. The simulation tests are implemented to verify that the SINS/GPS/ADS/DVL integrated navigation system can provide reliable navigation parameters when ADS and DVL are disabled. © 2021 Weiqi Li et al.
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