会议论文详细信息
International Conference on Mechanical Engineering, Automation and Control Systems 2015 | |
Low thrust spacecraft transfers optimization method with the stepwise control structure in the Earth-Moon system in terms of the L1-L2 transfer | |
机械制造;无线电电子学;计算机科学 | |
Fain, M.K.^1 ; Starinova, O.L.^1 | |
Samara State Aerospace University, 34, Moskovskoye shosse, Samara | |
443086, Russia^1 | |
关键词: Earth-Moon system; Flight time; Optimal controls; Optimization criteria; Optimization method; Pontryagin's maximum principle; Spacecraft transfers; Stepwise control; | |
Others : https://iopscience.iop.org/article/10.1088/1757-899X/124/1/012052/pdf DOI : 10.1088/1757-899X/124/1/012052 |
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学科分类:计算机科学(综合) | |
来源: IOP | |
【 摘 要 】
The paper outlines the method for determination of the locally optimal stepwise control structure in the problem of the low thrust spacecraft transfer optimization in the Earth-Moon system, including the L1-L2 transfer. The total flight time as an optimization criterion is considered. The optimal control programs were obtained by using the Pontryagin's maximum principle. As a result of optimization, optimal control programs, corresponding trajectories, and minimal total flight times were determined.
【 预 览 】
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