Gain-scheduled state feedback control design technique for flight vehicles

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For multi-input, multi-output (MIMO) nonlinearly parameter dependent linear parameter-varying (LPV) systems with multiple parameters, a design method of gain-scheduled state feedback control using a minimum sensitivity eigenvalue assignment of the frozen parameter closed-loop system with quadratic stability checks is proposed. The proposed design method is applied to the bank-to-turn (BTT) control of a flight vehicle, and the nonlinear 6 degree of freedom (DOF) simulations are performed to show the usefulness as a gain-scheduled state feedback control scheme.
Publisher
IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC
Issue Date
2001-01
Language
English
Article Type
Article
Keywords

PARAMETER-VARYING SYSTEMS; TRANSFORMATIONS

Citation

IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, v.37, no.1, pp.173 - 182

ISSN
0018-9251
URI
http://hdl.handle.net/10203/81343
Appears in Collection
EE-Journal Papers(저널논문)
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