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.
Gain-scheduled state feedback control design technique for flight vehicles
IEEE Transactions on Aerospace and Electronic Systems ; 37 , 1 ; 173-182
2001-01-01
405635 byte
Article (Journal)
Electronic Resource
English
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