A Novel Sensor Fault Detection in an Unmanned Quadrotor Based on Adaptive Neural Observer

被引:47
作者
Aboutalebi, Payam [1 ]
Abbaspour, Alireza [2 ]
Forouzannezhad, Parisa [2 ]
Sargolzaei, Arman [3 ]
机构
[1] Shahrood Univ Technol, Dept Elect Engn, Shahrood, Semnan, Iran
[2] Florida Int Univ, Dept Elect & Comp Engn, Miami, FL 33199 USA
[3] Florida Polytech Univ, Dept Elect Engn, Lakeland, FL USA
关键词
Malfunction; Sensor; Flight dynamic; Nonlinear model; Control; Extended Kalman Filter; NETWORK-BASED SENSOR; NONLINEAR-SYSTEMS; DYNAMIC INVERSION; IDENTIFICATION;
D O I
10.1007/s10846-017-0690-7
中图分类号
TP18 [人工智能理论];
学科分类号
081104 ; 0812 ; 0835 ; 1405 ;
摘要
Prompt detection and isolation of faults and failures in flight control systems are crucial to avoid negative impacts on human and environmental systems, and to the system itself. In this study, a new scheme based on a nonlinear dynamic model is designed for sensor fault detection and isolation in an unmanned aerial vehicle (UAV) system. In the proposed design, a neural network is used as an observer for faults in the UAV sensors. The weighting parameters of the neural network are updated by the Extended Kalman Filter (EKF). The designed fault detection (FD) system is applied to an unmanned quadrotor model, and the simulation results show that the proposed design is capable of the prompt detection of sensor faults.
引用
收藏
页码:473 / 484
页数:12
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