Title of article :
Model-based robust estimation and fault detection for MEMS-INS/GPS integrated navigation systems
Author/Authors :
Miao، نويسنده , , Lingjuan and Shi، نويسنده , , Jing، نويسنده ,
Issue Information :
روزنامه با شماره پیاپی سال 2014
Pages :
8
From page :
947
To page :
954
Abstract :
In micro-electro-mechanical system based inertial navigation system (MEMS-INS)/global position system (GPS) integrated navigation systems, there exist unknown disturbances and abnormal measurements. In order to obtain high estimation accuracy and enhance detection sensitivity to faults in measurements, this paper deals with the problem of model-based robust estimation (RE) and fault detection (FD). A filter gain matrix and a post-filter are designed to obtain a RE and FD algorithm with current measurements, which is different from most of the existing priori filters using measurements in one-step delay. With the designed filter gain matrix, the H-infinity norm of the transfer function from noise inputs to estimation error outputs is limited within a certain range; with the designed post-filter, the residual signal is robust to disturbances but sensitive to faults. Therefore, the algorithm can guarantee small estimation errors in the presence of disturbances and have high sensitivity to faults. The proposed method is evaluated in an integrated navigation system, and the simulation results show that it is more effective in position estimation and fault signal detection than priori RE and FD algorithms.
Keywords :
Fault detection , Integrated navigation , Inertial navigation systems , Micro-electro-mechanical system , robust estimation
Journal title :
Chinese Journal of Aeronautics
Serial Year :
2014
Journal title :
Chinese Journal of Aeronautics
Record number :
2265591
Link To Document :
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