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Discrete Sliding Mode Control for Hypersonic Cruise Missile
Joint Authors
Fan, Yong Hua
Yan, Peng Peng
Wang, Fan
Xu, Hong Yang
Source
Discrete Dynamics in Nature and Society
Issue
Vol. 2016, Issue 2016 (31 Dec. 2016), pp.1-9, 9 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2016-03-24
Country of Publication
Egypt
No. of Pages
9
Main Subjects
Abstract EN
A discrete variable structure control (DVSC) with sliding vector is presented to track the velocity and acceleration command for a hypersonic cruise missile.
In the design an integrator is augmented to ensure the tracking with zero steady-state errors.
Furthermore the sliding surface of acceleration is designed using the error of acceleration and acceleration rate to avoid the singularity of control matrix.
A proper power rate reaching law is utilized in this proposal; therefore the state trajectory from any initial point can be driven into the sliding surface.
Besides, in order to validate the robustness of controller, the unmolded dynamic and parameter disturbance of the missile are considered.
Through simulation the proposed controller demonstrates good performance in tracking velocity and acceleration command.
American Psychological Association (APA)
Fan, Yong Hua& Yan, Peng Peng& Wang, Fan& Xu, Hong Yang. 2016. Discrete Sliding Mode Control for Hypersonic Cruise Missile. Discrete Dynamics in Nature and Society،Vol. 2016, no. 2016, pp.1-9.
https://search.emarefa.net/detail/BIM-1103352
Modern Language Association (MLA)
Fan, Yong Hua…[et al.]. Discrete Sliding Mode Control for Hypersonic Cruise Missile. Discrete Dynamics in Nature and Society No. 2016 (2016), pp.1-9.
https://search.emarefa.net/detail/BIM-1103352
American Medical Association (AMA)
Fan, Yong Hua& Yan, Peng Peng& Wang, Fan& Xu, Hong Yang. Discrete Sliding Mode Control for Hypersonic Cruise Missile. Discrete Dynamics in Nature and Society. 2016. Vol. 2016, no. 2016, pp.1-9.
https://search.emarefa.net/detail/BIM-1103352
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1103352