2 DOF Robust Nonlinear Autopilot Design for a Small UAV using a Combination of Dynamic Inversion and H-Infinity Loop Shaping
AIAA Guidance, Navigation, and Control Conference and Exhibit
01.01.2005
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Missile Autopilot Designs Using H(infinity) Control with Gain scheduling and Dynamic Inversion
Online Contents | 1998
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