Abstract
This paper proposes a digital spacecraft overall power system design, simulation, analysis and verification mode, forming a unified simulation model based on a unified model, fully autonomously controllable, and the simulation results and power distribution map, grounding map and tasks time series is deeply integrated to realize the dynamic analysis and display of the whole satellite power supply and distribution system, as well as the digital flight of the ground test and the in-orbit flight process, and combined with a lunar probe model application example to carry out verification work. This has important guiding significance for the overall design and verification of the spacecraft.
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Xia, N., Du, Q., Liu, Z., Zhang, X., Chen, Y. (2020). The Digital Design and Verification of Overall Power System for Spacecraft. In: Liang, Q., Wang, W., Liu, X., Na, Z., Jia, M., Zhang, B. (eds) Communications, Signal Processing, and Systems. CSPS 2019. Lecture Notes in Electrical Engineering, vol 571. Springer, Singapore. https://doi.org/10.1007/978-981-13-9409-6_192
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DOI: https://doi.org/10.1007/978-981-13-9409-6_192
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