Beijing University of Aeronautics / I spa / Auburn University / Bar Coefficient / /
IndustryTerm
similar systems / gas flow / genetic algorithm / aerospace vehicle design minimum launch weight concepts / missile interceptor using genetic algorithms / design engineering applications / population-based computer algorithm / aerospace industry / launch systems / gas constant / recent heuristic search method / satellite launch vehicle propulsion system / time-efficient computer software / generated solutions / population size particle swarm optimization algorithm / satellite launch vehicle using hybrid optimization / power systems / aerospace vehicle dynamics / rocket motor metal cases / particle swarm optimization algorithm / space transportation vehicles / gas phase / satellite launch vehicle / food / artificial intelligence learning tool / /
Organization
Congress / Auburn University / School of Astronautics / Beijing University of Aeronautics and Astronautics / U.S. Air Force Research Lab/ Air Vehicle Directorate / National Aeronautics and Space Administration / Design Constraints Mission / /
Multidisciplinary design of air-launched satellite launch vehicle using particle swarm optimization