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Automatic control of a spacecraft transfer trajectory from an earth orbit to a moon orbit

被引：0
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作者：
Butu, Florentin-Alin [1 ]
Lungu, Romulus [2 ]
机构：
[1] University POLITEHNICA of Bucharest, Romania
[2] Faculty of Electrical Engineering, University of Craiova, Romania
来源：
UPB Scientific Bulletin, Series D: Mechanical Engineering | 2019年 / 81卷 / 01期
关键词：
Elliptical orbits - Keplerian parameters - Matlab/Simulink modeling - Non linear control - Nonlinear control laws - Reference orbit - Reference trajectories - Spacecraft transfers;
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页码：17 / 28
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