DocumentCode
2882105
Title
Observation and control for air-breathing hypersonic aircrafts based on sliding mode method
Author
Mu, Chaoxu ; Sun, Changyin ; Yu, Xinghuo
Author_Institution
Sch. of Autom., Southeast Univ., Nanjing, China
fYear
2011
fDate
7-10 Nov. 2011
Firstpage
3965
Lastpage
3970
Abstract
In this paper, the state observation and control problems are studied for air-breathing cruise hypersonic aircrafts. As many variables in flight cannot be measurable, a sliding mode observer is firstly introduced to derive all unmeasurable states. Secondly the feedback linearization is executed on the longitudinal model of air-breathing hypersonic aircrafts using all states, then a sliding mode controller is designed based on tracking errors, which guarantee the reachability condition in the sliding mode system and the stability of the whole system. Simulation results validate that the sliding mode observer can reproduce all unmeasurable states and the sliding mode controller can deal with the tracking control of velocity and altitude for air-breathing cruise hypersonic aircrafts.
Keywords
aircraft control; attitude control; control system synthesis; feedback; observers; reachability analysis; variable structure systems; velocity control; air-breathing cruise hypersonic aircraft control; altitude control; feedback linearization; reachability condition; sliding mode controller; sliding mode method; sliding mode observer; stability; state observation; tracking control; tracking errors; velocity control; Aerodynamics; Aerospace control; Aircraft; Atmospheric modeling; Equations; Mathematical model; Observers; Air-breathing hypersonic aircrafts; linearization; observation; sliding mode method; tracking control;
fLanguage
English
Publisher
ieee
Conference_Titel
IECON 2011 - 37th Annual Conference on IEEE Industrial Electronics Society
Conference_Location
Melbourne, VIC
ISSN
1553-572X
Print_ISBN
978-1-61284-969-0
Type
conf
DOI
10.1109/IECON.2011.6119957
Filename
6119957
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