Sliding Mode Control for Mass Moment Aerospace Vehicles Using Dynamic Inversion Approach
Joint Authors
Zhao, Yu-Xin
Zhang, Xiao-Yu
Xu, De-Xin
He, Kun-Peng
Source
Mathematical Problems in Engineering
Issue
Vol. 2013, Issue 2013 (31 Dec. 2013), pp.1-11, 11 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2013-10-28
Country of Publication
Egypt
No. of Pages
11
Main Subjects
Abstract EN
The moving mass actuation technique offers significant advantages over conventional aerodynamic control surfaces and reaction control systems, because the actuators are contained entirely within the airframe geometrical envelope.
Modeling, control, and simulation of Mass Moment Aerospace Vehicles (MMAV) utilizing moving mass actuators are discussed.
Dynamics of the MMAV are separated into two parts on the basis of the two time-scale separation theory: the dynamics of fast state and the dynamics of slow state.
And then, in order to restrain the system chattering and keep the track performance of the system by considering aerodynamic parameter perturbation, the flight control system is designed for the two subsystems, respectively, utilizing fuzzy sliding mode control approach.
The simulation results describe the effectiveness of the proposed autopilot design approach.
Meanwhile, the chattering phenomenon that frequently appears in the conventional variable structure systems is also eliminated without deteriorating the system robustness.
American Psychological Association (APA)
Zhang, Xiao-Yu& Zhao, Yu-Xin& Xu, De-Xin& He, Kun-Peng. 2013. Sliding Mode Control for Mass Moment Aerospace Vehicles Using Dynamic Inversion Approach. Mathematical Problems in Engineering،Vol. 2013, no. 2013, pp.1-11.
https://search.emarefa.net/detail/BIM-1031781
Modern Language Association (MLA)
Zhang, Xiao-Yu…[et al.]. Sliding Mode Control for Mass Moment Aerospace Vehicles Using Dynamic Inversion Approach. Mathematical Problems in Engineering No. 2013 (2013), pp.1-11.
https://search.emarefa.net/detail/BIM-1031781
American Medical Association (AMA)
Zhang, Xiao-Yu& Zhao, Yu-Xin& Xu, De-Xin& He, Kun-Peng. Sliding Mode Control for Mass Moment Aerospace Vehicles Using Dynamic Inversion Approach. Mathematical Problems in Engineering. 2013. Vol. 2013, no. 2013, pp.1-11.
https://search.emarefa.net/detail/BIM-1031781
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1031781