摘要
以四旋翼飞行器执行单元增益型故障的检测与重构为研究内容,设计基于滑模观测器的故障检测算法.针对飞行器姿态控制系统的驱动单元冗余特性,提出一种并行双降维观测器与超螺旋算法相结合的故障重构算法.对所提出的算法进行了理论分析,并通过数值仿真验证了所提出算法的有效性.
The fault detection and reconstruction method based on actutor gain-fault of a quad-rotor aircraft is proposed. A sliding-mode fault observer is designed to detect the fault. In consideration of the actuation redundancy characteristic, a fault reconstruction algorithm is proposed based on paralleled double-observers and a super-twisting algorithm. The theoretical analysis on the proposed methods is given, and the numerical simulation verifies the effectiveness of the proposed methods.
出处
《控制与决策》
EI
CSCD
北大核心
2015年第7期1214-1218,共5页
Control and Decision
基金
国家自然科学基金项目(61304017
11372309)
关键词
驱动单元故障检测
降维观测器
双观测器并行
超螺旋算法
actuator fault detection
reduced-order observer
paralleled double-observers
super-twisting algorithm