This paper presents an alternative techniques for computing linear feedback control law which stablize uncertain linear systems .Specifically, flight control system of aircraft and missiles which contains uncertain parameters. These un-certain parameters may be time varying. Their values, how, ever, are constrained to lie within known compact bounding sets. The main idea involves making Lyapunov derivative negative via a one- dimensional parameter, leading to solve algebraic Riccati equation. Several examples are included to demonstrate the importance of these techniques.
Kassem, W. (1989). ROBUST FLIGHT CONTROL FOR LINEAR SYSTEMS WITH TIME VARYING UNCERTAINTY. International Conference on Aerospace Sciences and Aviation Technology, 3(ASAT Conference 4-6 April 1989 , CAIRO), 821-834. doi: 10.21608/asat.1989.25951
MLA
Wahid M. Kassem. "ROBUST FLIGHT CONTROL FOR LINEAR SYSTEMS WITH TIME VARYING UNCERTAINTY", International Conference on Aerospace Sciences and Aviation Technology, 3, ASAT Conference 4-6 April 1989 , CAIRO, 1989, 821-834. doi: 10.21608/asat.1989.25951
HARVARD
Kassem, W. (1989). 'ROBUST FLIGHT CONTROL FOR LINEAR SYSTEMS WITH TIME VARYING UNCERTAINTY', International Conference on Aerospace Sciences and Aviation Technology, 3(ASAT Conference 4-6 April 1989 , CAIRO), pp. 821-834. doi: 10.21608/asat.1989.25951
VANCOUVER
Kassem, W. ROBUST FLIGHT CONTROL FOR LINEAR SYSTEMS WITH TIME VARYING UNCERTAINTY. International Conference on Aerospace Sciences and Aviation Technology, 1989; 3(ASAT Conference 4-6 April 1989 , CAIRO): 821-834. doi: 10.21608/asat.1989.25951
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