A Type Two Linearization Controller for a Resuable Launch Vehicle - A Singular Perturbation Approach
AIAA Atmospheric Flight Mechanics Conference and Exhibit
01.01.2004
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
AIAA-2004-5184 A Type Two Linearization Controller for a Resuable Launch Vehicle
British Library Conference Proceedings | 2004
|IMPROVED TRAJECTORY LINEARIZATION FLIGHT CONTROLLER FOR REUSABLE LAUNCH VEHICLES
British Library Conference Proceedings | 2004
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