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Study on the Technology of Spacecraft Dynamic Simulation and Emulation
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作者 WANG Hui GU Xue-mai 《Computer Aided Drafting,Design and Manufacturing》 2009年第1期17-25,共9页
To meet the requirements and functions of spacecraft dynamic simulation and emulation according to different flight periods, the realization of real time system with different configurations, control of the developmen... To meet the requirements and functions of spacecraft dynamic simulation and emulation according to different flight periods, the realization of real time system with different configurations, control of the development cycle and examples of application are presented in detail. On the basis of the satellite dynamic simulation technology, distributed network integrated with the component testing platforms is used to construct a multi-level bus network system. The system takes into full consideration the configuration flexibility, real time characteristics and extendibility. Test results show that both the software algorithm and the hardware integration of the system are correct and effective. The system could be used not only as the effective tool of designing and developing the components and whole assembly of satellites and missiles, but also for the dynamic simulation and emulation in all phases of a spacecraft development cycle. 展开更多
关键词 SPACECRAFT dynamic simulation and emulation distributed network real time
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