Sliding mode observer-based fault detection for helicopter system  

作　　者：M.Raghappriya S.Kanthalakshmi 

机构地区：[1]Department of Electronics and Instrumentation Engineering,Government College of Technology,Coimbatore,India [2]Department of Electrical and Electronics Engineering,PSG College of Technology,Coimbatore,India

出　　处：《Journal of Control and Decision》2023年第4期465-475,共11页控制与决策学报（英文）

摘　　要：Fault detection of non-linear systems is of great importance in control systems reliability.Undetected faults could lead to irreparable damage.This paper deals with fault diagnosis of helicopter system in the presence of uncertainties and disturbances.To deal with sensor,actuator and component faults,the observer-based diagnosis scheme which employs sliding mode observer is designed.Faults are modelled as an additive and multiplicative fault which is introduced as an abrupt and intermittent fault into the system.Observer inequality constraints and gain matrices are solved using a Lyapunov-based approach.The results display the effectiveness of the designed observer and the ability to handle faults.

关 键 词：Fault diagnosis sliding mode observer sensor actuator and component faults residual generation 

分 类 号：V275.1[航空宇航科学与技术—飞行器设计]