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Self healing control method against unmanned helicopter actuator stuck faults

机译:无人机执行器卡死故障的自愈控制方法

摘要

A self healing (SH) control framework is proposed in this paper against actuator stuck faults. For unmanned helicopters (UHs), the framework is composed by an active fault-tolerant control (FTC) system and reference redesign. The FTC system is based on linear-quadratic regulator (LQR) and pseudo inverse technique, which can compensate stuck faults of the post-fault system with output analytical redundancy (OAR) feature. The post-fault system may not achieve the original reference because remaining actuators' margin will degrade after stuck-fault compensation. A new reference is necessary for the post-fault system, which can be achieved by reference redesign method based on solving an optimal problem. At last the proposed SH framework is illustrated with a linear unmanned helicopter model, which includes rotor-speed control input and swashplate configuration. © 2014 IEEE.
机译:本文提出了一种针对执行器卡住故障的自愈(SH)控制框架。对于无人直升机(UH),该框架由主动容错控制(FTC)系统和参考重新设计组成。 FTC系统基于线性二次调节器(LQR)和伪逆技术,可利用输出分析冗余(OAR)功能补偿故障后系统的卡死故障。故障后系统可能无法获得原始参考,因为在执行故障补偿后,剩余的执行器裕度会降低。故障后系统需要一个新的参考,可以通过基于解决最优问题的参考重新设计方法来实现。最后用线性无人直升机模型说明了拟议的SH框架,该模型包括转子速度控制输入和斜盘配置。 ©2014 IEEE。

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