关于最大轨道转移问题

The Mathematica journal Pub Date : 2015-01-01 DOI:10.3888/TMJ.17-4

M. Muresan

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引用次数: 5

摘要

假设航天器在一个圆形轨道上运行，考虑在给定时间内以恒定推力使航天器能够转移到的最大可能圆形轨道的问题，变量参数为推力方向角β。同时假设在两个圆形轨道的共同中心只有一个引力中心。最后，假设所有常量和变量的归一化值。

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On the Maximal Orbit Transfer Problem

Assume that a spacecraft is in a circular orbit and consider the problem of finding the largest possible circular orbit to which the spacecraft can be transferred with constant thrust during a set time, so that the variable parameter is the thrust-direction angle β. Also assume that there is only one center of attraction at the common center of the two circular orbits. Finally, assume normalized values for all constants and variables.

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来源期刊

The Mathematica journal

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