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《Journal of Astronautics》 2001-04
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AN RAPID APPROACH FOR FLIGHT VEHICLE CONFIGURATION SCHEME SELECTION

Wang Shuhe 1 He Linshu 1 Ren Yanrong 2 Li Xiangqian 1 (1 The School of Space Technology of Beijing University of Aeronautics and Astronautics,Beijing 100083; 2 Institute of Mechanics,Chinese Academy of Sciences,Beijing 100080)  
This approach is composed of system fuzziness selection theory and orthogonal design method which based on the orthogonal table of statistics.An example is illustrated in this paper to show the usage of this method.The presented method is worthy to be considered using for the scheme selection of flight vehicles.
【CateGory Index】: V42
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