Integrated Power and Attitude Control Design of Satellites Based on a Fuzzy Adaptive Disturbance Observer Using Variable-Speed Control Moment Gyros
Joint Authors
Source
International Journal of Aerospace Engineering
Issue
Vol. 2016, Issue 2016 (31 Dec. 2016), pp.1-13, 13 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2016-03-23
Country of Publication
Egypt
No. of Pages
13
Abstract EN
To satisfy the requirements for small satellites that seek agile slewing with peak power, this paper investigates integrated power and attitude control using variable-speed control moment gyros (VSCMGs) that consider the mass and inertia of gimbals and wheels.
The paper also details the process for developing the controller by considering various environments in which the controller may be implemented.
A fuzzy adaptive disturbance observer (FADO) is proposed to estimate and compensate for the effects of equivalent disturbances.
The algorithms can simultaneously track attitude and power.
The simulation results illustrate the effectiveness of the control approach, which exhibits an improvement of 80 percent compared with alternate approaches that do not employ a FADO.
American Psychological Association (APA)
Chu, Zhongyi& Cui, Jing. 2016. Integrated Power and Attitude Control Design of Satellites Based on a Fuzzy Adaptive Disturbance Observer Using Variable-Speed Control Moment Gyros. International Journal of Aerospace Engineering،Vol. 2016, no. 2016, pp.1-13.
https://search.emarefa.net/detail/BIM-1105019
Modern Language Association (MLA)
Chu, Zhongyi& Cui, Jing. Integrated Power and Attitude Control Design of Satellites Based on a Fuzzy Adaptive Disturbance Observer Using Variable-Speed Control Moment Gyros. International Journal of Aerospace Engineering No. 2016 (2016), pp.1-13.
https://search.emarefa.net/detail/BIM-1105019
American Medical Association (AMA)
Chu, Zhongyi& Cui, Jing. Integrated Power and Attitude Control Design of Satellites Based on a Fuzzy Adaptive Disturbance Observer Using Variable-Speed Control Moment Gyros. International Journal of Aerospace Engineering. 2016. Vol. 2016, no. 2016, pp.1-13.
https://search.emarefa.net/detail/BIM-1105019
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1105019