| Autor: |
Da Jun Xu, Lin Shu He, S. Tauqeer ul Islam Rizvi |
| Rok vydání: |
2013 |
| Předmět: |
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| Zdroj: |
Applied Mechanics and Materials. 390:161-165 |
| ISSN: |
1662-7482 |
| DOI: |
10.4028/www.scientific.net/amm.390.161 |
| Popis: |
The multiphase numerical optimization study has been carried out for a 2-stage boost vehicle and small size X-33 type lifting-body reentry vehicle with heat rate and dynamic pressure constraint. The problem has been modeled as a nonlinear, multiphase optimal control problem with the objective to compute the optimum burn-out conditions as well as the best control deflections that would maximize the cross range performance of the boost-glide vehicle under study. The study has been performed using hp-adaptive Pseudospectral method. Comparative performance of the lifting-body vehicle with conventional ballistic missile trajectory has also been carried out. It has been found that for vehicle under study, and near maximum down range, the optimum burn-out angle is 13.6 degree which results in a cross-range of more than 100 km. |
| Databáze: |
OpenAIRE |
| Externí odkaz: |
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