Determination of Key Parameters for Reverse Engineering Solid Rocket Powered Missiles
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[1] Stephane Mondoloni,et al. AiAA-ga-4476 A GENETIC ALGORITHM FOR DETERMINING OPTIMAL FLIGHT TRAJECTORIES , 1998 .
[2] Roy J. Hartfield,et al. Optimizing a Solid Rocket Motor Boosted Ramjet Powered Missile Using a Genetic Algorithm , 2005 .
[3] Rhonald M. Jenkins,et al. Design of an air to air interceptor using genetic algorithms , 1999 .
[4] Ciann-Dong Yang,et al. Applications of Genetic-Taguchi Algorithm in Flight Control Designs , 2005 .
[5] J. Billheimer,et al. Optimization and design simulation in solid rocket design , 1968 .
[6] Luciano Blasi,et al. THE OPTIMIZATION OF GAS TURBINE ENGINE DESIGN BY GENETIC ALGORITHMS1 , 2000 .
[7] Kamran Behdinan,et al. AIRCRAFT CONCEPTUAL DESIGN USING GENETIC ALGORITHMS , 2000 .
[8] Jongsoo Lee,et al. Genetic algorithm based design of transonic airfoils using Euler equations , 2000 .
[9] Stephen D. Heister,et al. Application of Genetic Algorithms to the optimization of hybrid rockets , 1998 .