引用本文: | 牛云.椭圆弹道射程角和飞行时间公式的一种推导方法.[J].国防科技大学学报,1990,12(2):55-57.[点击复制] |
Niu Yun.A Method for Deducing the Formulas of the Range Angle and the Flying Time with the Elliptical Orbit[J].Journal of National University of Defense Technology,1990,12(2):55-57[点击复制] |
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椭圆弹道射程角和飞行时间公式的一种推导方法 |
牛云 |
(89740部队)
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摘要: |
本文利用椭圆弹道长轴方向有一常量的性质,计算了被动段弹道的射程和飞行时间。 |
关键词: 能量守恒,角动量守恒,被动段,射程角,飞行时间 |
DOI: |
投稿日期:1989-08-05 |
基金项目: |
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A Method for Deducing the Formulas of the Range Angle and the Flying Time with the Elliptical Orbit |
Niu Yun |
(89740 Unit)
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Abstract: |
The range angle and the flying time for the passive section are calculated by using the quality with a constant vector in the direction of the major axis of the elliptical orbit in this paper. |
Keywords: energy conservation,angular momentum conservation,passive section,flying time,range angle |
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