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
2005-01-01
Conference paper
Electronic Resource
English
Missile Autopilot Designs Using H(infinity) Control with Gain scheduling and Dynamic Inversion
Online Contents | 1998
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