Three-Axes Missile Autopilot Design: From Linear to Nonlinear Control Strategies
Author:
Affiliation:
1. Aerospatiale Matra Missiles, 92323 Chatillon CEDEX, France Supelec, 91192 Gif-sur-Yvette, France
2. Aerospatiale Matra Missiles, 92323 Chatillon CEDEX, France
3. Supelec, 91192 Gif-sur-Yvette, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.4676
Reference30 articles.
1. 4Scorletti, G. “Approche Unifie de l’Analyse et de la Commande par Formulation LMI,” Ph.D. Dissertation,Univ. Paris XI, Orsay, France, 1997.
2. Gain-scheduled missile autopilot design using linear parameter varying transformations
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