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The Two-Point Boundary-Value Problem for Rocket Trajectories
The two dimensional gravity turn problem is addressed allowing for the effects of variable rocket mass due to propellant consumption, thrust and thrust vector angle, lift and drag forces at an angle-of-attack and atmospheric mass density varying with altitude; Coriolis and centrifugal forces are neg...
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| 主要な著者: | , |
|---|---|
| フォーマット: | Artigo |
| 言語: | Inglês |
| 出版事項: |
MDPI AG
2020-09-01
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| シリーズ: | Aerospace |
| 主題: | |
| オンライン･アクセス: | https://www.mdpi.com/2226-4310/7/9/131 |
| タグ: |
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