Nonlinear Output Regulation with Input Delay and Application in AHV Attitude Control
Joint Authors
Source
International Journal of Aerospace Engineering
Issue
Vol. 2017, Issue 2017 (31 Dec. 2017), pp.1-14, 14 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2017-05-08
Country of Publication
Egypt
No. of Pages
14
Abstract EN
Time delay phenomena exist almost everywhere in the actual world and are especially important in the control of an AHV.
The small time delay usually ignored in control may cause quite obvious errors in the flight trajectory tracking, because of the extremely high flight speed.
In this paper, a new framework of solving a nonlinear input delay regulation problem is proposed for the first time, which is comprised of nonlinear damping controllers, nonlinear disturbance observers, and a nonlinear time delay predictor-based compensator, under the proved separation principle.
Then the attitude tracking control of an AHV with a known time-varying input delay is studied based on the proposed design framework.
Simulation results show the advantage of the proposed control method.
American Psychological Association (APA)
Cai, Liang& Wu, Qingxian. 2017. Nonlinear Output Regulation with Input Delay and Application in AHV Attitude Control. International Journal of Aerospace Engineering،Vol. 2017, no. 2017, pp.1-14.
https://search.emarefa.net/detail/BIM-1158152
Modern Language Association (MLA)
Cai, Liang& Wu, Qingxian. Nonlinear Output Regulation with Input Delay and Application in AHV Attitude Control. International Journal of Aerospace Engineering No. 2017 (2017), pp.1-14.
https://search.emarefa.net/detail/BIM-1158152
American Medical Association (AMA)
Cai, Liang& Wu, Qingxian. Nonlinear Output Regulation with Input Delay and Application in AHV Attitude Control. International Journal of Aerospace Engineering. 2017. Vol. 2017, no. 2017, pp.1-14.
https://search.emarefa.net/detail/BIM-1158152
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1158152