角速度约束下飞机姿态稳定

IECON 2020 The 46th Annual Conference of the IEEE Industrial Electronics Society Pub Date : 2020-10-18 DOI:10.1109/IECON43393.2020.9254830

Bo Yu, Linan Wang, Haibo Du, Jun Zhou, Di Wu, Shihong Ding

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引用次数: 0

摘要

本文主要研究航天器的姿态控制问题。系统模型中不仅考虑了角速度约束，而且考虑了外界干扰。在该控制器的作用下，姿态可以收敛到期望值，角速度可以渐近收敛到原点。

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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Attitude stabilization for aircraft under angular velocity constraint

This paper mainly investigates the attitude control problem for a spacecraft. Not only angular velocity constraint but also external disturbances are considered in the system model. Under the action of proposed controller, the posture can be converged to the desired value, and the angular velocity can be asymptotically converged to the origin.

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IECON 2020 The 46th Annual Conference of the IEEE Industrial Electronics Society

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