控制理论(社会学)
航天器
稳健性(进化)
姿态控制
扰动(地质)
计算机科学
跟踪(教育)
控制工程
惯性参考系
控制(管理)
工程类
人工智能
物理
心理学
古生物学
教育学
生物化学
化学
量子力学
生物
基因
航空航天工程
作者
Zean Bao,Maobin Lu,Fang Deng
标识
DOI:10.1016/j.ifacol.2023.10.005
摘要
In this paper, we consider the attitude tracking and disturbance rejection problem of uncertain flexible spacecrafts. Compared with existing works, we consider two types of uncertainties of flexible spacecrafts, that is, the uncertain parameters of the inertial matrix, and the unknown external disturbance with unbounded energy. Inspired by the internal model principle, we design a class of dynamic compensators and some auxiliary dynamic systems to compensate the external disturbance. Then, by introducing a series of coordinate transformations, we convert the attitude tracking and disturbance rejection problem into an adaptive regulation problem of an augmented system. Finally, we design the adaptive control law and show that attitude tracking of uncertain flexible spacecrafts can be achieved in the presence of unknown disturbances. The effectiveness and robustness of the controller are illustrated by some numerical simulations.
科研通智能强力驱动
Strongly Powered by AbleSci AI