Optimal Multi-Orbit Trajectories for Inserting a Low-Thrust Spacecraft to a High Elliptic Orbit

V. G. Petukhov

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Optimal Multi-Orbit Trajectories for Inserting a Low-Thrust Spacecraft to a High Elliptic Orbit

机译：将低推力航天器插入高椭圆轨道的最优多轨道轨迹

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摘要

The results of numerical optimization of multi-orbit trajectories of the transfer of a low-thrust spacecraft to a high elliptic orbit are presented. An analysis of characteristics of the optimal transfers including their structure is performed. The methods of description of the structures of optimal multi-orbit trajectories are suggested with the goal of their classification.

机译：给出了低推力航天器向高椭圆轨道转移的多轨道轨迹的数值优化结果。对最佳转移的特征（包括其结构）进行了分析。以分类为目标，提出了描述最佳多轨道轨迹结构的方法。

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来源
《Cosmic research》 |2009年第3期|243-250|共8页
作者
V. G. Petukhov;
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作者单位

Khrunichev State Research and Production Space Center, Moscow;

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原文格式 PDF
正文语种 eng
中图分类
关键词
ballistics (projectiles; rockets);

机译：弹道学（弹丸;火箭）;

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专利

1. Numerical Solutions to Exact Equations of Motion along Near-Optimal Multi-Orbit Trajectories for a Spacecraft in a Newtonian Gravitational Field [J] . B. N. Kiforenko, I. Yu. Vasiliev Cosmic research . 2011,第5期

机译：牛顿引力场中航天器沿最优轨道的精确运动方程的数值解
2. Planar Problem of an Optimal Transfer of a Low-Thrust Spacecraft from High-Elliptic to Geosynchronous Orbit [J] . R. Z. Akhmetshin Cosmic research . 2004,第3期

机译：低推力航天器从高椭圆轨道到地球同步轨道最优转移的平面问题
3. Analysis of Evolution of Multi-Orbit Perturbed Trajectories of a Spacecraft in a Central Field of Attraction [J] . V. V. Laricheva Cosmic research . 2013,第4期

机译：引力中心场中航天器多轨道摄动轨迹的演化分析
4. Evolutionary algorithms to optimize low-thrust trajectory design in spacecraft orbital precession mission [C] . Abolfazl Shirazi, Josu Ceberio, Jose A. Lozano IEEE Congress on Evolutionary Computation . 2017

机译：优化航天器轨道进动任务低推力轨迹设计的进化算法
5. Optimal low-thrust transfer trajectories from Earth to Earth-Moon L2 point halo orbits. [D] . Starchville, Thomas Francis, Jr. 1996

机译：从地球到月球L2点光晕轨道的最佳低推力转移轨迹。
6. A Submillimeter-Level Relative Navigation Technology for Spacecraft Formation Flying in Highly Elliptical Orbit [O] . Xiaoliang Wang, Deren Gong, Yifei Jiang, 2020

机译：高度椭圆轨道上飞船形成飞行的海底级相对导航技术
7. Multi-Step Optimization Strategy for Fuel-Optimal Orbital Transfer of Low-Thrust Spacecraft [O] . M. Rasotto, R. Armellin, P. Di Lizia 2016

机译：低推力航天器燃料最优轨道转移的多步优化策略

Optimal Multi-Orbit Trajectories for Inserting a Low-Thrust Spacecraft to a High Elliptic Orbit

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