Abstract
For the propulsion technology and orbit transfer control of low-thrust spacecraft, the previous traditional methods and technologies are relatively expensive and cannot guarantee the optimal solution. This paper proposes a new solution method for the low-thrust spacecraft propulsion technology and orbit transfer design, which can optimize the propulsion and orbit transfer flight of low-thrust spacecraft. Theoretical design shows that this method can quickly obtain the optimal analytical solution, and has good optimization effects on the propulsion and orbit transfer of low-thrust spacecraft.
| Original language | English |
|---|---|
| Title of host publication | Proceedings of the 43rd Chinese Control Conference, CCC 2024 |
| Editors | Jing Na, Jian Sun |
| Publisher | IEEE Computer Society |
| Pages | 3761-3766 |
| Number of pages | 6 |
| ISBN (Electronic) | 9789887581581 |
| DOIs | |
| Publication status | Published - 2024 |
| Event | 43rd Chinese Control Conference, CCC 2024 - Kunming, China Duration: 28 Jul 2024 → 31 Jul 2024 |
Publication series
| Name | Chinese Control Conference, CCC |
|---|---|
| ISSN (Print) | 1934-1768 |
| ISSN (Electronic) | 2161-2927 |
Conference
| Conference | 43rd Chinese Control Conference, CCC 2024 |
|---|---|
| Country/Territory | China |
| City | Kunming |
| Period | 28/07/24 → 31/07/24 |
Keywords
- Low-thrust spacecraft
- electric propulsion technology
- optimal control
- orbit transfer
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Han, S., Mo, B., Li, W., & Jin, B. (2024). A Low-thrust Spacecraft Propulsion Technology and Its Orbit Transfer Application. In J. Na, & J. Sun (Eds.), Proceedings of the 43rd Chinese Control Conference, CCC 2024 (pp. 3761-3766). (Chinese Control Conference, CCC). IEEE Computer Society. https://doi.org/10.23919/CCC63176.2024.10661584