In this paper, a flight control law for a simplified F-14 aircraft model is designed based on variable structure control (VSC) theory. For m-input, q-output linear uncertain systems (q
Variable structure robust flight control system for the F-14
IEEE Transactions on Aerospace and Electronic Systems ; 33 , 1 ; 77-84
1997-01-01
1489869 byte
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Variable Structure Robust Flight Control System for the F-14
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