Nonlinear Robust Missile Autopilot Design Using Successive Galerkin Approximation
Nonlinear Robust Missile Autopilot Design Using Successive Galerkin Approximation
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Nonlinear Robust Missile Autopilot Design Using Successive Galerkin Approximation
Guidance, navigation, and control conference ; 1999 ; Portland; OR
Guidance, navigation, and control conference ; 3950-4068 ; 384-391
PAPERS- AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS ; 1 , 3950-4068
1999-01-01
8 pages
Cover title: A collection of the AIAA guidance, navigation, and control conference technical papers
Conference paper
English
guidance , navigation , AIAA
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