Plant inversion control of tail-controlled missiles
Guidance, Navigation, and Control Conference ; 1997 ; New Orleans , LA , U.S.A.
01.01.1997
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Adaptive Control Based on a Parametric Affine Model for Tail-Controlled Missiles
Online Contents | 2006
|AIAA-2006-6569 Optimal Control Solution for Dual (Tail and Canard) Controlled Missiles
British Library Conference Proceedings | 2006
|