Fuel Minimizing Control for Constrained Relative Satellite Orbits
In this paper, we study the fuel minimization problem of hovering satellite subject to a practical constraint on the trajectory of the deputy satellite. It is first shown that the constraint condition can be expressed equivalently as maximum flight time inequalities. On this basis, a cost function r...
| Main Authors: | , , , |
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| Other Authors: | |
| Format: | Conference Paper |
| Published: |
Guiyang University
2010
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| Subjects: | |
| Online Access: | http://hdl.handle.net/20.500.11937/28100 |
| _version_ | 1848752444897492992 |
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| author | Gao, X. Teo, Kok Lay Sun, Y. Duan, G. |
| author2 | Honglei Xu |
| author_facet | Honglei Xu Gao, X. Teo, Kok Lay Sun, Y. Duan, G. |
| author_sort | Gao, X. |
| building | Curtin Institutional Repository |
| collection | Online Access |
| description | In this paper, we study the fuel minimization problem of hovering satellite subject to a practical constraint on the trajectory of the deputy satellite. It is first shown that the constraint condition can be expressed equivalently as maximum flight time inequalities. On this basis, a cost function relating to the fuel burn is formulated. A numerical procedure is developed to solve this fuel minimization problem. |
| first_indexed | 2025-11-14T08:08:44Z |
| format | Conference Paper |
| id | curtin-20.500.11937-28100 |
| institution | Curtin University Malaysia |
| institution_category | Local University |
| last_indexed | 2025-11-14T08:08:44Z |
| publishDate | 2010 |
| publisher | Guiyang University |
| recordtype | eprints |
| repository_type | Digital Repository |
| spelling | curtin-20.500.11937-281002023-01-13T07:56:32Z Fuel Minimizing Control for Constrained Relative Satellite Orbits Gao, X. Teo, Kok Lay Sun, Y. Duan, G. Honglei Xu Xinmin Yang Wei Wei fuel burn Relative satellite orbits constrained orbits optimal control fuel minimizing cost function In this paper, we study the fuel minimization problem of hovering satellite subject to a practical constraint on the trajectory of the deputy satellite. It is first shown that the constraint condition can be expressed equivalently as maximum flight time inequalities. On this basis, a cost function relating to the fuel burn is formulated. A numerical procedure is developed to solve this fuel minimization problem. 2010 Conference Paper http://hdl.handle.net/20.500.11937/28100 Guiyang University fulltext |
| spellingShingle | fuel burn Relative satellite orbits constrained orbits optimal control fuel minimizing cost function Gao, X. Teo, Kok Lay Sun, Y. Duan, G. Fuel Minimizing Control for Constrained Relative Satellite Orbits |
| title | Fuel Minimizing Control for Constrained Relative Satellite Orbits |
| title_full | Fuel Minimizing Control for Constrained Relative Satellite Orbits |
| title_fullStr | Fuel Minimizing Control for Constrained Relative Satellite Orbits |
| title_full_unstemmed | Fuel Minimizing Control for Constrained Relative Satellite Orbits |
| title_short | Fuel Minimizing Control for Constrained Relative Satellite Orbits |
| title_sort | fuel minimizing control for constrained relative satellite orbits |
| topic | fuel burn Relative satellite orbits constrained orbits optimal control fuel minimizing cost function |
| url | http://hdl.handle.net/20.500.11937/28100 |