Alternative Formulations for Transient Dynamic Response Optimization
Author:
Affiliation:
1. University of Iowa, Iowa City, Iowa 52242
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.12045
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2. 2Haug, E. J., and Arora, J. S., Applied Optimum Design, Mechanical and Structural Systems, Wiley, New York, 1979, pp.348-354.
3. Optimum design of systems for dynamics and controls using sequentialquadratic programming
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