地球同步转移轨道设计:一种实用方法

E. Hernandez, J. Bolivar, Q. Wang
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引用次数: 5

摘要

本文提出了一种实用的地球同步转移轨道设计方法。利用Hohmann转移轨道、Keppler第三定律和推进剂消耗方程设计了注入轨道和地球同步轨道之间的中间轨道。根据设计,在这些中间轨道之后将有一颗通信卫星在其轨道机动序列中确保其最终轨道位置和最小的燃料消耗。仿真结果和与STK软件的比较表明,该方法可以简单有效地用于地球同步转移轨道设计。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Geosynchronous transfer orbit design: A practical approach
This paper is proposing a practical approach for a Geosynchronous Transfer Orbit design. To design the intermediate orbits between the injection orbit and the Geosynchronous Orbit were used the Hohmann Transfer Orbit, Keppler 3rd Law and the propellant consumption equations. According to design, these intermediate orbits will be followed by a communication satellite during its orbital maneuver sequence ensuring its final orbital position and minimal fuel consumption. Simulation results and comparison with STK software showed that the approach can simply and effectively be used in the Geosynchronous Transfer Orbit Design.
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