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Initial Values Determination of Thrust Parameters for Continuously Low-Thrust Maneuvering Spacecraft.

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Bibliographic Details
Title: Initial Values Determination of Thrust Parameters for Continuously Low-Thrust Maneuvering Spacecraft.
Authors: Guo, Wen1, Tao, Xuefeng1, Hu, Min1, humin@hgd.edu.cn, Xue, Wen1
Source: Applied Sciences (2076-3417); Jul2025, Vol. 15 Issue 14, p8064, 22p
Database: Applied Science & Technology Source
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ISSN:20763417
DOI:10.3390/app15148064