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西北工业大学 国内
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A shape-based method for continuous low-thrust trajectory design between circular coplanar orbits
Qun Fang, Xuefeng Wang, Chong Sun,
Jianping Yuan
航天学院
Northwestern Polytechnical University Xian
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Engineering
Free Case
100%
Thrust Direction
100%
Fourier Series
100%
Coplanar Circular Orbit
100%
Low Earth Orbit
50%
Initial Guess
50%
Flight Time
50%
Optimal Control
50%
Physics
Control Theory
100%
Optimal Control
100%
Flight Time
100%
Trajectory Optimization
100%