基于Fliess 泛函展开式的航天器姿态控制

Abstract

Abstract: The paper surveys the attitude tracking of aircrafts via Fliess functional expansion. First, one step and ¯nite step predictive controls are considered. Then we show that when the system decoupling matrix is of full row rank, using a proper state feedback, the closed-loop system has a Fliess functional expansion with only ¯nite terms. This approach is particularly suitable for the online design of attitude control of spacecraft.

Key words: attitude control, Fliess functional expansion, decoupling matrix, output tracking

CLC Number:

o231

CHENG Daizhan , YUAN Yanyan, QIAO Yupeng. Attitude Control of Spacecraft via Fliess Functional Expansion[J]., 2009, 35(1): 3-6.

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Attitude Control of Spacecraft via Fliess Functional Expansion

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