Angle maneuver control strategy of spacecraft based on momentum wheel system with component synthesi

来源 :The 4th International Conference on Dynamics, Vibration and | 被引量 : 0次 | 上传用户：zhaojian1990

【摘要】

：

【作者】

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Guanyu Wang Weiping Ge Zhigang Zhao Guangwei Yang

【机构】

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School of Mechanical engineering, Harbin Institute of Technology

【出处】

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The 4th International Conference on Dynamics, Vibration and

【发表日期】

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2014年8期

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An angle maneuver control strategy of spacecraft with flexible structure based on component synthesis vibration suppression(CSVS) method is put forward.Unwanted flexible vibration modes can be eliminated while desired rigid motion can be achieved by this method.Momentum wheel system is used as the actuator of the spacecraft s angle maneuver.The DC motor control method is researched in order to combine momentum wheel system with CSVS method.

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