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Design of Flight Control System for a Novel Tilt-Rotor UAV
Joint Authors
Source
Issue
Vol. 2020, Issue 2020 (31 Dec. 2020), pp.1-14, 14 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2020-03-13
Country of Publication
Egypt
No. of Pages
14
Main Subjects
Abstract EN
This paper presents the control system design process of a novel tilt-rotor unmanned aerial vehicle (TRUAV).
First, a new configuration scheme with the tilting rotors is designed.
Then, the detailed nonlinear mathematical model is established, and the parameters are acquired from designed experiments and numerical analyses.
For control design purposes, the dynamics equation is linearized around the hovering equilibrium point, and a control allocation method based on trim calculation is developed.
To deal with the actuator saturation and uncertain disturbance problems for the novel TRUAV, an improved flight control law based on the combination of the robust servo linear quadratic regulator (RSLQR) optimal control and the extended state observer (ESO) is proposed.
The designed flight control law has a simple structure with a high reliability in engineering.
Simulations and hovering flight tests are carried out to verify the effectiveness of the mathematical model and the proposed control strategy.
American Psychological Association (APA)
Chen, Zaibin& Jia, Hongguang. 2020. Design of Flight Control System for a Novel Tilt-Rotor UAV. Complexity،Vol. 2020, no. 2020, pp.1-14.
https://search.emarefa.net/detail/BIM-1142072
Modern Language Association (MLA)
Chen, Zaibin& Jia, Hongguang. Design of Flight Control System for a Novel Tilt-Rotor UAV. Complexity No. 2020 (2020), pp.1-14.
https://search.emarefa.net/detail/BIM-1142072
American Medical Association (AMA)
Chen, Zaibin& Jia, Hongguang. Design of Flight Control System for a Novel Tilt-Rotor UAV. Complexity. 2020. Vol. 2020, no. 2020, pp.1-14.
https://search.emarefa.net/detail/BIM-1142072
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1142072