TY - JOUR
T1 - Model-based robust estimation and fault detection for MEMS-INS/GPS integrated navigation systems
AU - Miao, Lingjuan
AU - Shi, Jing
N1 - Publisher Copyright:
© 2014 Production and hosting by Elsevier Ltd.
PY - 2014/8/1
Y1 - 2014/8/1
N2 - 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.
AB - 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.
KW - Fault detection
KW - Inertial navigation systems
KW - Integrated navigation
KW - Micro-electro-mechanical
KW - Robust estimation
KW - system
UR - http://www.scopus.com/inward/record.url?scp=84908069881&partnerID=8YFLogxK
U2 - 10.1016/j.cja.2014.06.012
DO - 10.1016/j.cja.2014.06.012
M3 - Article
AN - SCOPUS:84908069881
SN - 1000-9361
VL - 27
SP - 947
EP - 954
JO - Chinese Journal of Aeronautics
JF - Chinese Journal of Aeronautics
IS - 4
ER -