TY - GEN
T1 - Sensor fault diagnosis of GPS/INS tightly coupled navigation system based on state chi-square test and improved simplified fuzzy ARTMAP neural network
AU - Liu, Chang
AU - Wang, Honglun
AU - Li, Na
AU - Yu, Yue
N1 - Publisher Copyright:
© 2017 IEEE.
PY - 2017/7/2
Y1 - 2017/7/2
N2 - In order to improve the reliability of GPS/INS tightly coupled navigation system, a novel sensor fault diagnosis scheme combined with the advantages of state chi-square test (SCST) and simplified fuzzy ARTMAP neural network (SFAM) is presented in this paper. Firstly, in order to overcome the problem of fault detection in noisy environment, a two state propagator based on SCST is applied in the navigation system to detect single fault to multiple faults of different sensors (gyroscope, accelerometer and GPS receiver). Then, traditional grey wolf optimizer is improved by adding a memory influence term in the update formula and a 'greedy strategy' to enhance new individual's fitness. A simplified fuzzy ARTMAP neural network optimized by improved grey wolf optimizer is employed to classify sensor fault according to SCST result. Meanwhile, another improved simplified fuzzy ARTMAP neural network is employed to identify the fault magnitude and fault occurring time. Further, faults features base on SCST results corresponding to different sensors and different flight trajectories are analyzed. The analysis results are used to design fault classification and identification scheme. Finally, simulations which take into account all fault types, different fault magnitude, and different flight trajectories are given. The simulation results show that the proposed fault diagnosis method can detect, classify, and identify the sensor fault of GPS/INS navigation system.
AB - In order to improve the reliability of GPS/INS tightly coupled navigation system, a novel sensor fault diagnosis scheme combined with the advantages of state chi-square test (SCST) and simplified fuzzy ARTMAP neural network (SFAM) is presented in this paper. Firstly, in order to overcome the problem of fault detection in noisy environment, a two state propagator based on SCST is applied in the navigation system to detect single fault to multiple faults of different sensors (gyroscope, accelerometer and GPS receiver). Then, traditional grey wolf optimizer is improved by adding a memory influence term in the update formula and a 'greedy strategy' to enhance new individual's fitness. A simplified fuzzy ARTMAP neural network optimized by improved grey wolf optimizer is employed to classify sensor fault according to SCST result. Meanwhile, another improved simplified fuzzy ARTMAP neural network is employed to identify the fault magnitude and fault occurring time. Further, faults features base on SCST results corresponding to different sensors and different flight trajectories are analyzed. The analysis results are used to design fault classification and identification scheme. Finally, simulations which take into account all fault types, different fault magnitude, and different flight trajectories are given. The simulation results show that the proposed fault diagnosis method can detect, classify, and identify the sensor fault of GPS/INS navigation system.
UR - https://www.scopus.com/pages/publications/85050007559
U2 - 10.1109/ROBIO.2017.8324800
DO - 10.1109/ROBIO.2017.8324800
M3 - 会议稿件
AN - SCOPUS:85050007559
T3 - 2017 IEEE International Conference on Robotics and Biomimetics, ROBIO 2017
SP - 2527
EP - 2532
BT - 2017 IEEE International Conference on Robotics and Biomimetics, ROBIO 2017
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2017 IEEE International Conference on Robotics and Biomimetics, ROBIO 2017
Y2 - 5 December 2017 through 8 December 2017
ER -