Flight Control Law Design for a Flexible Aircraft: Limits of Performance
Author:
Affiliation:
1. ONERA, F-31055 Toulouse CEDEX, France
2. AIRBUS France, 31060 Toulouse CEDEX 03, 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/10.2514/1.18535
Reference24 articles.
1. Multiobjective control: an overview
2. Robust H Design for Lateral Flight Control of Highly Flexible Aircraft
3. Linear Parameter-Varying Modeling and Control of Structural Dynamics with Aerothermoelastic Effects
4. Mixed-norm H2/L1 controller synthesis via fixed-order dynamic compensation: A Riccati equation approach
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