Design of a flight control system for a highly maneuverable aircraft using robust dynamic inversion
Guidance, Navigation, and Control Conference ; 1994 ; Scottsdale , AZ , U.S.A.
01.01.1994
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Design of a Flight Control System for a Highly Maneuverable Aircraft Using Robust Dynamic Inversion
British Library Conference Proceedings | 1994
|Robust Dynamic Inversion for Control of Highly Maneuverable Aircraft
Online Contents | 1995
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