NDLI: Tracking control of air-breathing hypersonic aircrafts in cruising flight based on sliding mode method

Content Provider	IEEE Xplore Digital Library
Author	Mu Chaoxu Wang Bin Sun Changyin Yu Xinghuo
Copyright Year	2011
Description	Author affiliation: Platform Technologies Research Institute, RMIT University, Melbourne, Victoria 3000, Australia (Wang Bin) \|\| School of Automation, Southeast University, Nanjing, Jiangsu 210096, China (Mu Chaoxu; Sun Changyin; Yu Xinghuo)
Abstract	Due to nonlinear coupling and complex fight dynamics, the control of hypersonic aircrafts is usually challenging. In this paper, taking the longitudinal motion of a general air-breathing hypersonic aircraft as the controlled object, we designed a sliding mode controller to control velocity and altitude tracking based on input-output linearization. The velocity and altitude subsystems can be obtained by linearization and highest order derivatives of outputs in the two subsystems are designed to satisfy the sufficient and necessary condition of sliding mode control based on Lyapunov functions. A saturation function is used in the sliding mode controller to reduce chattering instead of the discontinuous sign function. Simulation is studied to validate that the controller based on sliding mode can make the aircraft system stable and meet the desired tracking performance.
Starting Page	5245
Ending Page	5249
File Size	303718
Page Count	5
File Format	PDF
ISBN	9781457706776
ISSN	21612927
e-ISBN	9789881725592
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2011-07-22
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	Chinese Assoc of Automati
Subject Keyword	Atmospheric modeling Air-breathing hypersonic aircraft Input-output linearization Chattering Aerodynamics Military aircraft Mathematical model Aircraft Vehicle dynamics Sliding mode control Aerospace control
Content Type	Text
Resource Type	Article

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