Aircraft design for mission performance using nonlinear multiobjective optimization methods
- 1 December 1990
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 27 (12) , 1043-1049
- https://doi.org/10.2514/3.45979
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Multiobjective optimization in structural design with uncertain parameters and stochastic processesAIAA Journal, 1984
- Systematic Control Design by Optimizing a Vector Performance IndexIFAC Proceedings Volumes, 1979
- On implementation of the extended interior penalty functionInternational Journal for Numerical Methods in Engineering, 1976