NDLI: Control of Hypersonic Vehicle Based on Improved QFT

Content Provider	IEEE Xplore Digital Library
Author	Shi Zhen Wang Fei Ma Wen-qiao
Copyright Year	2012
Abstract	Hypersonic vehicle has high military value in terms of real-time reconnaissance, remote rapid deployment and precision strike, especially the implementation of real-time reconnaissance mission has unique advantages. Efficient thrust, the aircraft must be flying high dynamic pressure conditions, in order to control the resulting aerodynamic heating and aerodynamic drag for the hypersonic vehicle angle of attack for precise control, at the same time, the dynamic characteristics of the hypersonic vehicle conventional aircraft are very different, the most critical aerodynamic characteristics are good enough stability of the pre-degree in terms of the control system must have a very strong robust feedback system. the QFT method, using an improved design of hypersonic flight longitudinal channel controller, Simulation results show that the robust controller design meets the system requirements.
Starting Page	227
Ending Page	230
File Size	186931
Page Count	4
File Format	PDF
ISBN	9781467326469
DOI	10.1109/ISCID.2012.64
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2012-10-28
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	hepersonic Aerodynamics Control systems Robustness control system nonlinear Aircraft Vehicle dynamics QFT Vehicles Aerospace control
Content Type	Text
Resource Type	Article

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