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- W2382793669 abstract "The objective of the whole-spacecraft isolation is to reduce the launch-induced dynamic loads and the quality control cost of the satellite and its components,as well as increase the launch reliability,by insertion of isolators between the satellite and the launch vehicle.An adaptive hybrid genetic algorithm is proposed in this paper to optimize stiffness and damping of the isolators.Comparison of the frequency response analysis results shows that the optimized whole-spacecraft isolation system more effectively reduces spacecraft axial / lateral response due to the broadband structure-born launch environment.The case of the whole-spacecraft isolation optimization design demonstrates the efficiency,validity and availability of the genetic algorithm." @default.
- W2382793669 created "2016-06-24" @default.
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- W2382793669 date "2005-01-01" @default.
- W2382793669 modified "2023-09-23" @default.
- W2382793669 title "Optimization Design of the Whole-Spacecraft Isolation System" @default.
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