Reaction-Jet Missile Autopilot Design Based on Adaptive Fuzzy Sliding Mode Control via Backstepping
AIAA Guidance, Navigation, and Control Conference
01.01.2009
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
AUTOPILOT DESIGN FOR AN AGILE MISSILE USING L1 ADAPTIVE BACKSTEPPING CONTROL
British Library Conference Proceedings | 2012
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