Attitude control of a satellite using the SDRE method

Proceedings of the 1997 American Control Conference (Cat. No.97CH36041) Pub Date : 1997-06-04 DOI:10.1109/ACC.1997.609665

D. Parrish, D. Ridgely

引用次数: 60

Abstract

Examines the use of nonlinear regulation for attitude control of a satellite controlled by internal momentum rotors. Specifically, the nonlinear method using the state dependent Riccati equation (SDRE) developed by Cloutier, D'Souza, and Mracek (1996) is applied and examined under numerical simulations.

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利用SDRE方法进行卫星姿态控制

研究了由内动量转子控制的卫星姿态控制的非线性调节。具体来说，应用了Cloutier、D’souza和Mracek(1996)提出的状态依赖里卡蒂方程(SDRE)的非线性方法，并在数值模拟中进行了检验。

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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来源期刊

Proceedings of the 1997 American Control Conference (Cat. No.97CH36041)

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