Nonlinear multidisciplinary design optimization using system identification and optimal control theory

DOI10.1016/0045-7825(95)00899-3zbMath0862.73038OpenAlexW2076790329MaRDI QIDQ2365155

K. Appa, J. H. Argyris

Publication date: 22 January 1997

Published in: Computer Methods in Applied Mechanics and Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0045-7825(95)00899-3

zbMATH Keywords

constraintsmodal coordinatesflying vehiclesgeneralized state space coordinatesmultiple objective functions

Mathematics Subject Classification ID

System identification (93B30) Optimization problems in solid mechanics (74P99)

Related Items (1)

Synergistic aircraft design using CFD air loads

Cites Work

• Hermes space shuttle: Exploration of reentry aerodynamics
• Some considerations on the natural approach
• Aerodynamic design optimization using sensitivity analysis and computational fluid dynamics
• New successive approximation method for optimum structural design
• Detailed study of complex flow fields of aerodynamical configurations by using numerical methods.
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