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Vibration control of flexible spacecraft actuated by piezoceramics via variable structure strategy

哈尔滨工业大学学报(英文版)2007,Vol.14Issue(5):604-608,5.
哈尔滨工业大学学报(英文版)2007,Vol.14Issue(5):604-608,5.

Vibration control of flexible spacecraft actuated by piezoceramics via variable structure strategy

Vibration control of flexible spacecraft actuated by piezoceramics via variable structure strategy

1

作者信息

  • 1. Dept.of Control Science & Engineering,Harbin Institute of Technology,Harbin 150001,China;Dept.of Control Science & Engineering,Harbin Institute of Technology,Harbin 150001,China
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摘要

Abstract

This paper presented a hybrid control scheme to vibration reduction of flexible spacecraft during rotational maneuver by using variable structure output feedback control(VSOFC)and piezoelectric materials. The control configuration included the attitude controller based on VSOFC method and vibration attenuator designed by constant-gain negative velocity feedback control. The attitude controller consisted of a linear feedback term and a discontinuous feedback term. With the presence of this attitude controller, an additional flexible control system acting on the flexible parts can be designed for vibration control. Compared with conventional proportional-derivative(PD)control, the developed control scheme guarantees not only the stability of the closed-loop system, but also yields better performance and robustness in the presence of parametric uncertainties and external disturbance. Simulation results are presented for the spacecraft model to show the effectiveness of the proposed control techniques.

关键词

vibration suppression/flexible spacecraft/variable structure output feedback control/attitude maneuver

Key words

vibration suppression/flexible spacecraft/variable structure output feedback control/attitude maneuver

分类

航空航天

引用本文复制引用

..Vibration control of flexible spacecraft actuated by piezoceramics via variable structure strategy[J].哈尔滨工业大学学报(英文版),2007,14(5):604-608,5.

基金项目

Sponsored by Program for Young Excellent Talents in Harbin Institute of Technology(Grant No.HITQNJS.2007.001),National Natural Science Foundation of China(Grant No.60674101)and Research Fund for the Doctoral Program of Higher Education of China(Grant No.20050213010). (Grant No.HITQNJS.2007.001)

哈尔滨工业大学学报(英文版)

1005-9113

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