NDLI: Speed control for aircraft based on nonlinear adaptive backstepping technology

Content Provider	IEEE Xplore Digital Library
Author	Zhiwei Guo Cheng Peng Yong Wang
Copyright Year	2010
Description	Author affiliation: Department of Automation, University of Science and Technology of China, Hefei, Anhui, China (Zhiwei Guo; Cheng Peng; Yong Wang)
Abstract	According to the characteristics of the aircraft velocity vector, the velocity vector control problem is investigated. The relative degree is 2 for the speed, which is related to the virtual control input (the aircraft angular rate). The speed second-order differential equation is transformed into two first-order differential equations. By combining these two equations with an angle rate equation, the cascade condition for backstepping technology is satisfied. Then, a control law for speed and angle of sideslip tracking is designed using adaptive backstepping control, and a parameter estimation law is also given based on Lyapunov method. The mentioned control law and parameter estimation law can guarantee that the speed and angle of sideslip tracking error asymptotically converges to zero. The numerical simulation results based on F16 nonlinear model show the effectiveness of the proposed algorithm.
Starting Page	2565
Ending Page	2571
File Size	896322
Page Count	7
File Format	PDF
ISBN	9781424467129
e-ISBN	9781424467129
DOI	10.1109/WCICA.2010.5554630
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2010-07-07
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Backstepping Aerospace control Aircraft Differential equations Equations Mathematical model Velocity control relative degree aircraft adaptive backstepping control speed control
Content Type	Text
Resource Type	Article

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