NDLI: Parametric approach for longitudinal attitude control of a hypersonic vehicle

Content Provider	IEEE Xplore Digital Library
Author	Duan Guangren Hu Yanmei Tan Feng Liu Wangkui
Copyright Year	2015
Description	Author affiliation: Harbin Inst. of Technol., Harbin, China (Duan Guangren; Hu Yanmei; Tan Feng; Liu Wangkui)
Abstract	In this paper, a parametric approach for longitudinal attitude control of a hypersonic vehicle is presented. Firstly, according to the complicated aerodynamics characteristic of a hypersonic vehicle, the model of the pitch channel is treated as an interval system in order to cope with parameter uncertainties. Secondly, by employing robust stability analysis and parametric control theory, a parameterization of state feedback controllers for the interval autopilot system is obtained. Thirdly, by appropriately optimizing the free parameters in the robust stabilizing controller, the $H_{2}$ norm of the disturbance-output transfer function is made sufficiently small over the system parameter intervals. A simulation example of the pitch channel of a hypersonic vehicle demonstrates that the system achieves good performance with external disturbance despite the aerodynamical parameters vary in a large scale.
Starting Page	5776
Ending Page	5781
File Size	11447179
Page Count	6
File Format	PDF
ISBN	9789881563897
ISSN	19341768
DOI	10.1109/ChiCC.2015.7260541
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2015-07-28
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	Technical Committee on Control Theory, Chinese Association of Automation
Subject Keyword	Disturbance Attenuation Attitude control Robust Stabilization Aerodynamics Attenuation Robustness Hypersonic Vehicle Vehicle dynamics Optimization Vehicles Parametric Approach
Content Type	Text
Resource Type	Article

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