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Attitude and Altitude Controller Design for Quad-Rotor Type MAVs
Joint Authors
Weng, Liguo
Xia, Min
Wang, Wei
Ma, Hao
Ye, Xuefei
Source
Mathematical Problems in Engineering
Issue
Vol. 2013, Issue 2013 (31 Dec. 2013), pp.1-9, 9 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2013-05-09
Country of Publication
Egypt
No. of Pages
9
Main Subjects
Abstract EN
Micro air vehicles (MAVs) have a wide application such as the military reconnaissance, meteorological survey, environmental monitoring, and other aspects.
In this paper, attitude and altitude control for Quad-Rotor type MAVs is discussed and analyzed.
For the attitude control, a new method by using three gyroscopes and one triaxial accelerometer is proposed to estimate the attitude angle information.
Then with the approximate linear model obtained by system identification, Model Reference Sliding Mode Control (MRSMC) technique is applied to enhance the robustness.
In consideration of the relatively constant altitude model, a Linear Quadratic Gaussian (LQG) controller is adopted.
The outdoor experimental results demonstrate the superior stability and robustness of the controllers.
American Psychological Association (APA)
Wang, Wei& Ma, Hao& Xia, Min& Weng, Liguo& Ye, Xuefei. 2013. Attitude and Altitude Controller Design for Quad-Rotor Type MAVs. Mathematical Problems in Engineering،Vol. 2013, no. 2013, pp.1-9.
https://search.emarefa.net/detail/BIM-1032000
Modern Language Association (MLA)
Wang, Wei…[et al.]. Attitude and Altitude Controller Design for Quad-Rotor Type MAVs. Mathematical Problems in Engineering No. 2013 (2013), pp.1-9.
https://search.emarefa.net/detail/BIM-1032000
American Medical Association (AMA)
Wang, Wei& Ma, Hao& Xia, Min& Weng, Liguo& Ye, Xuefei. Attitude and Altitude Controller Design for Quad-Rotor Type MAVs. Mathematical Problems in Engineering. 2013. Vol. 2013, no. 2013, pp.1-9.
https://search.emarefa.net/detail/BIM-1032000
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1032000