Output Feedback Variable Structure Adaptive Control Approach to Missile Autopilot Design
AIAA Guidance, Navigation, and Control Conference ; 2011 ; Portland , Oregon
01.01.2011
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Output Feedback Variable Structure Adaptive Control Approach to Missile Autopilot Design
British Library Conference Proceedings | 2011
|ICAS2016_0474: MISSILE AUTOPILOT DESIGN USING CONTRACTION THEORY-BASED OUTPUT FEEDBACK CONTROL
British Library Conference Proceedings | 2016
|A Robust Adaptive Nonlinear Control Approach to Missile Autopilot Design
British Library Conference Proceedings | 1999
|Discrete Variable Structure Controller for Missile Autopilot
British Library Conference Proceedings | 2002
|