Title :
Parametrically varying flight control system design with full block scalings
Author :
Scherer, C.W. ; Njio, R.G.E. ; Bennani, S.
Author_Institution :
Mech. Eng. Syst. & Control Group, Delft Univ. of Technol., Netherlands
Abstract :
A systematic procedure for synthesizing a parametrically varying controller for nonlinear systems is presented and applied to a high performance flight control system of a tail-fin controlled missile. The strongly nonlinear and parameter dependent system has to be stabilized and must exhibit high performance over a large operating range
Keywords :
control system synthesis; missile control; nonlinear control systems; stability; full block scalings; high-performance flight control system; nonlinear systems; parameter dependent system; parametrically varying flight control system design; stabilization; tail-fin controlled missile; Aerospace control; Control system synthesis; Control systems; Design optimization; Nonlinear control systems; Nonlinear systems; Robust control; Stability; Time varying systems; Uncertainty;
Conference_Titel :
Decision and Control, 1997., Proceedings of the 36th IEEE Conference on
Conference_Location :
San Diego, CA
Print_ISBN :
0-7803-4187-2
DOI :
10.1109/CDC.1997.657686
