NDLI: A novel method of vibration suppression for multi-modal flexible spacecraft

Content Provider	IEEE Xplore Digital Library
Author	Zhao Lin Wu Xiaowen Hao Yong Zhang Haizhu
Copyright Year	2014
Description	Author affiliation: Harbin Veic Technol. Dev. Co., Harbin, China (Zhang Haizhu) \|\| Coll. of Autom., Harbin Eng. Univ., Harbin, China (Zhao Lin; Wu Xiaowen; Hao Yong)
Abstract	In order to reduce the vibration of the flexible attachments, a combined control strategy based on input shaping and a PD adaptive feedback control is proposed. The multi-modal flexible attachments will create the vibration in the attitude maneuvers, therefore the spacecraft with imaging function cannot insure the image quality. In allusion to this problem, the multi-modal input shaper is designed to improve stability which based on the vibration frequency and damping ratio of the entire closed-loop system. Considering the control system of attitude dynamics structure and the uncertainty parameter, a PD adaptive feedback control is used. From the simulation results it can be seen that the proposed control strategy can quickly reduce the flexible attachments vibration and improve the performance of closed-loop system.
Starting Page	8822
Ending Page	8825
File Size	631406
Page Count	4
File Format	PDF
ISBN	9789881563873
ISSN	19341768
DOI	10.1109/ChiCC.2014.6896484
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2014-07-28
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	TCCT, CAA
Subject Keyword	Vibrations Space vehicles Damping Flexible vibration Uncertainty Attitude control adaptive PD control Input Shaping PD control Mathematical model multi-modal
Content Type	Text
Resource Type	Article

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