Control-Structure Integrated Design with Closed-Form Design Metrics Using Physical Programming
Author:
Affiliation:
1. Northeastern University, Boston, Massachusetts 02115
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.447
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1. Integrated aircraft-controller design using linear matrix inequalities
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