Aircraft design for mission performance using nonlinear multiobjective optimization methods
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[1] G. Kreisselmeier,et al. SYSTEMATIC CONTROL DESIGN BY OPTIMIZING A VECTOR PERFORMANCE INDEX , 1979 .
[2] R. C. Feagin,et al. Delta method, an empirical drag buildup technique , 1978 .
[3] Gregory A. Wrenn,et al. An indirect method for numerical optimization using the Kreisselmeir-Steinhauser function , 1989 .
[4] William C. Davidon,et al. Variable Metric Method for Minimization , 1959, SIAM J. Optim..
[5] Charles Gide,et al. Cours d'économie politique , 1911 .
[6] N. A. Radovcich,et al. Some experiences in aircraft aeroelastic design using Preliminary Aeroelastic Design of Structures (PAD) , 1984 .
[7] Uri Kirsch,et al. Multilevel Approach to Optimum Structural Design , 1975 .
[8] Singiresu S Rao,et al. Multiobjective optimization in structural design with uncertain parameters and stochastic processes , 1984 .
[9] J. Cassis,et al. On implementation of the extended interior penalty function. [optimum structural design] , 1976 .
[10] C. D. Mote,et al. Optimization methods for engineering design , 1971 .
[11] S. M. Sliwa,et al. OPDOT: A computer program for the optimum preliminary design of a transport airplane , 1980 .
[12] Lotfi A. Zadeh,et al. Optimality and non-scalar-valued performance criteria , 1963 .
[13] P. Kokotovic,et al. Optimal tension regulation of a strip winding process , 1970 .
[14] Jaroslaw Sobieszczanski-Sobieski,et al. A new algorithm for general multiobjective optimization , 1988 .