DocumentCode :
646287
Title :
Robustness analysis of feedback linearisation with robust state estimation for a nonlinear missile model
Author :
Norton, Peter ; Prempain, Emmanuel
Author_Institution :
Dept. of Eng., Univ. of Leicester, Leicester, UK
fYear :
2013
fDate :
17-19 July 2013
Firstpage :
4220
Lastpage :
4225
Abstract :
A nonlinear missile model with time-varying uncertain parameters is controlled with a simple feedback linearisation and time-scale separation design, with synthesis based on the nominal model and full state feedback. The closed-loop system is then represented as a linear fractional transformation (LFT). A robust H filter is designed for the controlled plant, to estimate unknown states. Robust stability of the closed-loop system is then verified by using a scaled linear differential inclusion (LDI) technique.
Keywords :
H filters; closed loop systems; control system synthesis; linearisation techniques; missile control; nonlinear control systems; robust control; state estimation; state feedback; LDI technique; LFT; closed-loop system; controlled plant; feedback linearisation; linear fractional transformation; nominal full state feedback model; nonlinear missile model; robust H filter design; robust stability; robustness analysis; scaled linear differential inclusion technique; time-scale separation design; time-varying uncertain parameters; unknown state estimation; Actuators; Closed loop systems; Linear matrix inequalities; Robust stability; Robustness; Stability analysis; Uncertainty;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference (ECC), 2013 European
Conference_Location :
Zurich
Type :
conf
Filename :
6669695
Link To Document :
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