Constrained Optimization of Launch Vehicle Trajectory Using Spline and Bezier Curves
Design of launch vehicle (LV) trajectory is among the problems in which the use of optimization is of high significance. Implementing optimization using optimal control problem leads to a two point boundary value problem (TPBVS) that can be solved only numerically. On the other hand, development of...
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| Principais autores: | , , , |
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| Formato: | Artigo |
| Idioma: | Persa |
| Publicado em: |
Aerospace Research Institute
2010-01-01
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| coleção: | فصلنامه علوم و فناوری فضایی |
| Assuntos: | |
| Acesso em linha: | https://jsst.ias.ir/article_14384_8ea9f4f95a8d75f0e7dd96cbc7b27644.pdf |
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