Hybrid Low Thrust Propulsion Trajectory Design and Optimization Using Virtual Gravity Method
a novel spacecraft trajectory design method using hybrid low thrust system is proposed in this paper. The hybrid system is constituted with a solar sail propulsion thruster and a solar electric propulsion thruster. In proposed method, the former one provides radical thrust and circumferential thrust...
| Format: | Article |
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| Language: | zho |
| Published: |
The Northwestern Polytechnical University
2018-08-01
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| Series: | Xibei Gongye Daxue Xuebao |
| Subjects: | |
| Online Access: | https://www.jnwpu.org/articles/jnwpu/pdf/2018/04/jnwpu2018364p618.pdf |