Optimal Low Thrust Orbit Transfer Using Direct Collocation Method
In this paper, a new approach is proposed for solving the problem of optimal low thrust orbit transfer. In this approach, the problem of trajectory optimization of optimal orbit transfer is defined by modified equinoctial orbital elements. For solving this problem, direct collocation method, that is...
Gorde:
| Egile Nagusiak: | , |
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| Formatua: | Artigo |
| Hizkuntza: | Persa |
| Argitaratua: |
Aerospace Research Institute
2008-12-01
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| Saila: | فصلنامه علوم و فناوری فضایی |
| Gaiak: | |
| Sarrera elektronikoa: | https://jsst.ias.ir/article_14368_0f96103d8e7885222207fd2775eeba79.pdf |
| Etiketak: |
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