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Indirect Adaptive Attitude Control for a Ducted Fan Vertical Takeoff and Landing Microaerial Vehicle
Joint Authors
Sheng, Shouzhao
Sun, Chenwu
Zhao, Hong
Source
Mathematical Problems in Engineering
Issue
Vol. 2015, Issue 2015 (31 Dec. 2015), pp.1-11, 11 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2015-08-03
Country of Publication
Egypt
No. of Pages
11
Main Subjects
Abstract EN
The present paper addresses an attitude tracking control problem of a ducted fan microaerial vehicle.
The proposed indirect adaptive controller can greatly reduce tracking error in the initial stage of the adaptive learning process by using an error compensation strategy and can achieve good capability to eliminate the adverse effect of measurement noises on the convergence of adjustable parameters.
Moreover, the learning rate adaptation strategy is proposed to further minimize the adverse effect of large learning rates on the convergence of adjustable parameters.
The experimental tests have illustrated the effectiveness of the proposed adaptive controller.
American Psychological Association (APA)
Sheng, Shouzhao& Sun, Chenwu& Zhao, Hong. 2015. Indirect Adaptive Attitude Control for a Ducted Fan Vertical Takeoff and Landing Microaerial Vehicle. Mathematical Problems in Engineering،Vol. 2015, no. 2015, pp.1-11.
https://search.emarefa.net/detail/BIM-1072971
Modern Language Association (MLA)
Sheng, Shouzhao…[et al.]. Indirect Adaptive Attitude Control for a Ducted Fan Vertical Takeoff and Landing Microaerial Vehicle. Mathematical Problems in Engineering No. 2015 (2015), pp.1-11.
https://search.emarefa.net/detail/BIM-1072971
American Medical Association (AMA)
Sheng, Shouzhao& Sun, Chenwu& Zhao, Hong. Indirect Adaptive Attitude Control for a Ducted Fan Vertical Takeoff and Landing Microaerial Vehicle. Mathematical Problems in Engineering. 2015. Vol. 2015, no. 2015, pp.1-11.
https://search.emarefa.net/detail/BIM-1072971
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1072971