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- W2360804265 abstract "This paper discusses the six-degree-freedom mathematical modeling and simulation method for Launch Vehicle's flight control system based on Distributed Interactive Simulation Technology (DIST), designs digital simulation algorithm and simulation system." @default.
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- W2360804265 date "2003-01-01" @default.
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- W2360804265 title "Research on Distributed Interactive Simulation Technology of Launch Vehicle's Control System" @default.
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