High Accuracy Attitude Control System Design for Satellite with Flexible Appendages
Joint Authors
Wu, Zhi-Gang
Wang, Haixu
Ruan, Zhengwei
Wang, Enmei
Zhou, Wenya
Source
Mathematical Problems in Engineering
Issue
Vol. 2014, Issue 2014 (31 Dec. 2014), pp.1-6, 6 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2014-11-04
Country of Publication
Egypt
No. of Pages
6
Main Subjects
Abstract EN
In order to realize the high accuracy attitude control of satellite with flexible appendages, attitude control system consisting of the controller and structural filter was designed.
When the low order vibration frequency of flexible appendages is approximating the bandwidth of attitude control system, the vibration signal will enter the control system through measurement device to bring impact on the accuracy or even the stability.
In order to reduce the impact of vibration of appendages on the attitude control system, the structural filter is designed in terms of rejecting the vibration of flexible appendages.
Considering the potential problem of in-orbit frequency variation of the flexible appendages, the design method for the adaptive notch filter is proposed based on the in-orbit identification technology.
Finally, the simulation results are given to demonstrate the feasibility and effectiveness of the proposed design techniques.
American Psychological Association (APA)
Zhou, Wenya& Wang, Haixu& Ruan, Zhengwei& Wu, Zhi-Gang& Wang, Enmei. 2014. High Accuracy Attitude Control System Design for Satellite with Flexible Appendages. Mathematical Problems in Engineering،Vol. 2014, no. 2014, pp.1-6.
https://search.emarefa.net/detail/BIM-1046393
Modern Language Association (MLA)
Zhou, Wenya…[et al.]. High Accuracy Attitude Control System Design for Satellite with Flexible Appendages. Mathematical Problems in Engineering No. 2014 (2014), pp.1-6.
https://search.emarefa.net/detail/BIM-1046393
American Medical Association (AMA)
Zhou, Wenya& Wang, Haixu& Ruan, Zhengwei& Wu, Zhi-Gang& Wang, Enmei. High Accuracy Attitude Control System Design for Satellite with Flexible Appendages. Mathematical Problems in Engineering. 2014. Vol. 2014, no. 2014, pp.1-6.
https://search.emarefa.net/detail/BIM-1046393
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1046393