Bi-elliptic Transfer Between Coplanar Circular Orbits

版本 1.1.0.0 (492.1 KB) 作者: David Eagle
Bi-elliptic orbital transfer between two coplanar circular Earth orbits.
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更新时间 2013/7/9

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This is a MATLAB script that can be used to determine the characteristics of a three impulse bi-elliptic transfer between two coplanar circular orbits. The impulsive assumption means that the velocity, but not the position, of the space vehicle is changed instantaneously.

引用格式

David Eagle (2024). Bi-elliptic Transfer Between Coplanar Circular Orbits (https://www.mathworks.com/matlabcentral/fileexchange/38885-bi-elliptic-transfer-between-coplanar-circular-orbits), MATLAB Central File Exchange. 检索来源 .

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版本 已发布 发行说明
1.1.0.0

Added three-dimensional trajectory graphics and a graphical primer vector analysis. Updated PDF document to reflect these new features.
1.0.0.0