Autopilot design for a tail-controlled missile using two-degree-of-freedom controllers
Guidance, Navigation, and Control Conference ; 1995 ; Baltimore , MD , U.S.A.
01.01.1995
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Linearization of a Six-Degree-of-Freedom Missile for Autopilot Analysis
Online Contents | 1998
|Autopilot for a Nonlinear Non-Minimum Phase Tail-Controlled Missile (AIAA 2014-1293)
British Library Conference Proceedings | 2014
|