Direct approach to the analysis of control reversal and its sensitivity
Author:
Affiliation:
1. Politecnico di Milano, Milan, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.10510
Reference7 articles.
1. Optimality criteria and mathematical programming in structural weight optimization
2. Preliminary Design of Composite Wings for Buckling, Strength, and Displacement Constraints
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