Attitude control of a satellite using the SDRE method

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作者
Parrish, DK
Ridgely, DB
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TP [自动化技术、计算机技术];
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0812 ;
摘要
This paper 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 [1], will be applied and examined under numerical simulations.
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页码:942 / 946
页数:5
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