NDLI: Robust tracking control for the hypersonic flight vehicle via backstepping method

Content Provider	IEEE Xplore Digital Library
Author	Yao Yu Qian Zhang Junwei Wang Chang-Yin Sun
Copyright Year	2014
Description	Author affiliation: Sch. of Autom. & Electr. Eng., Univ. of Sci. & Technol. Beijing, Beijing, China (Yao Yu; Junwei Wang; Chang-Yin Sun) \|\| Sch. of Electr. Eng. & Comput. Sci., Louisiana State Univ., Baton Rouge, LA, USA (Qian Zhang)
Abstract	The problem of output tracking control is addressed for the longitudinal dynamics of a generic hypersonic flight vehicle. For the altitude subsystem and velocity subsystem, the dynamics is transformed into block-triangular form where the backstepping scheme is used. This problem is challenging due to the nonlinear uncertain complex interactions between the altitude and velocity subsystems. A new design approach of robust controller is proposed by combining standard backstepping with signal compensation method. It is shown that semiglobal robust stability and semiglobal robust practical tracking property of the closed-loop system can be ensured and the tracking error can be made as small as desired.
Starting Page	4306
Ending Page	4311
File Size	228732
Page Count	6
File Format	PDF
ISBN	9789881563873
ISSN	19341768
DOI	10.1109/ChiCC.2014.6895661
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2014-07-28
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	TCCT, CAA
Subject Keyword	Robust control Uncertainty Backstepping Nonlinear Hypersonic vehicle Robust Robustness MIMO Mathematical model Vehicle dynamics Vehicles
Content Type	Text
Resource Type	Article

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4	Project PI / Joint PI	Principal Investigator and Joint Principal Investigators of the project	Dr. B. Sutradhar bsutra@ndl.gov.in Prof. Saswat Chakrabarti will be added soon
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