Fault-Tolerant Attitude Tracking Control for Satellite Based on Event-Triggered Training

Baomin Li, Kenan Yong, Shuyi Shao
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Abstract

In this work, the fuzzy logic system (FLS)-based fault-tolerant attitude tracking control scheme is developed for the satellite under the backstepping framework. Specifically, the FLSs are introduced to approximate the unknown actuator fault. In order to take advantage of the high intelligence component, the training of the FLSs is proceeded in the ground base station. Meanwhile, since the actuator fault possesses the sudden property, the event-triggered training mechanism is employed for the FLSs. Namely, only when the actuator fault causes the output of the controlled system to fail to meet the user-specified tracking performance, the weight of the FLSs used to approximate the unknown fault will be updated. Thus, the developed control scheme is capable of saving communication resource and reducing communication burden of the satellite. The stability of the closed-loop system is proved by using the Lyapunov function method. Finally, the simulation example shows the effectiveness of the designed control scheme.
基于事件触发训练的卫星容错姿态跟踪控制
本文提出了一种基于模糊逻辑系统(FLS)的反步框架下的卫星容错姿态跟踪控制方案。具体地说,引入fls来近似执行器的未知故障。为了充分发挥高智能组件的优势,在地面基站中对FLSs进行训练。同时,由于执行器故障具有突发性,采用事件触发训练机制对执行器进行训练。即,只有当执行器故障导致被控系统的输出不能满足用户指定的跟踪性能时,用于近似未知故障的fls的权值才会更新。因此,所开发的控制方案能够节省通信资源,减轻卫星的通信负担。利用李雅普诺夫函数方法证明了闭环系统的稳定性。最后,通过仿真实例验证了所设计控制方案的有效性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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