卫星的滑模姿态控制

2017 International Conference on Engineering & MIS (ICEMIS) Pub Date : 2017-05-08 DOI:10.1109/ICEMIS.2017.8273046

M. Benenia, M. Benslama

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引用次数: 1

摘要

本文主要研究卫星姿态控制问题。该控制方法基于鲁棒滑模控制。设计了一种滑模控制器，使系统的状态变量收敛到期望值。其中控制器参数可以驱动状态撞击滑动面。介绍了控制设计的步骤。

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 control of a satellite using sliding mode

This paper is dedicated to the problem of a satellite attitude control. The control method is based upon a robust sliding mode control. A sliding mode controller has been designed in such a way that the state variables of the system converge to the desired values. Where the controller parameters can drive the state to hit the sliding surface. The steps of the control design are presented.

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来源期刊

2017 International Conference on Engineering & MIS (ICEMIS)

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