A Method for Deducing the Formulas of the Range Angle and the Flying Time with the Elliptical Orbit
Author:
Affiliation:
Fund Project:
摘要
|
图/表
|
访问统计
|
参考文献
|
相似文献
|
引证文献
|
资源附件
|
文章评论
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。
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.
参考文献
相似文献
引证文献
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. 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.