A Multiconstrained Ascent Guidance Method for Solid Rocket-Powered Launch Vehicles
This study proposes a multiconstrained ascent guidance method for a solid rocket-powered launch vehicle, which uses a hypersonic glide vehicle (HGV) as payload and shuts off by fuel exhaustion. First, pseudospectral method is used to analyze the two-stage launch vehicle ascent trajectory with differ...
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| Autors principals: | , |
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| Format: | Artigo |
| Idioma: | Inglês |
| Publicat: |
Wiley
2016-01-01
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| Col·lecció: | International Journal of Aerospace Engineering |
| Accés en línia: | http://dx.doi.org/10.1155/2016/6346742 |
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