Optimization of the Transfer Trajectory of a Low-Thrust Spacecraft for Research of Jupiter Using an Earth Gravity-Assist Maneuver

M.S. Konstantinov; A. A. Orlov

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Optimization of the Transfer Trajectory of a Low-Thrust Spacecraft for Research of Jupiter Using an Earth Gravity-Assist Maneuver

机译：利用地球重力辅助技术优化木星研究用低推力航天器的转移轨迹

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摘要

The paper analyzes the possibility of the use of a gravity-assist maneuver for flight to Jupiter. The advantage of the Earth gravity-assist maneuver in comparison with the direct transfer in terms of reduction of amount of energy required per transfer is considered. Quantitative and qualitative evaluations of two transfer profiles are given.

机译：本文分析了使用重力辅助机动飞行到木星的可能性。考虑到地球重力辅助操纵与直接传递相比在减少每次传递所需能量方面的优势。给出了两种转移曲线的定量和定性评估。

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来源
《Solar system research》 |2014年第7期|606-612|共7页
作者
M.S. Konstantinov; A. A. Orlov;
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作者单位

Moscow Aviation Institute, Moscow, Russia;

Lavochkin Research and Production Association, Khimki, Moscow oblast, Russia;

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收录信息美国《科学引文索引》(SCI);
原文格式 PDF
正文语种 eng
中图分类
关键词
spacecraft; gravity-assist maneuver; trajectory optimization;

机译：航天器重力辅助动作轨迹优化;

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1. Technique of Optimizing Trajectories of Interplanetary Transfers with Gravity Assisted Maneuvers Using Low-Thrust Propulsion [J] . Orlov A. A. Cosmic research . 2019,第5期

机译：低推力重力辅助机动优化行星际转移轨迹的技术
2. Evolutionary Neurocontrol: A Novel Method for Low-Thrust Gravity-Assist Trajectory Optimization [J] . Ian Carnelli, Bernd Dachwald, Massimiliano Vasile Journal of Guidance, Control, and Dynamics . 2009,第2期

机译：进化神经控制：一种低推力重力辅助弹道优化的新方法
3. Evolutionary Neurocontrol: A Novel Method for Low-Thrust Gravity-Assist Trajectory Optimization [J] . Ian Carnelli, Bernd Dachwalc, Massimiliano Vasile Journal of guidance, control, and dynamics . 2009,第2期

机译：进化神经控制：一种低推力重力辅助弹道优化的新方法
4. Optimal-Fuel, Low-Thrust Earth-Ivar Transfer Trajectory with Venus Gravity-Assist [C] . 1st International Symposium on Systems and Control in Aerospace and Astronautics （ISSCAA 2006）论文集 . 2006

机译：金星重力辅助下的最佳燃料，低推力土-伊瓦特转移轨迹
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. An Automated Solution of the Low-Thrust Interplanetary Trajectory Problem [O] . Jacob A. Englander, Bruce A. Conway -1

机译：低推力行星际轨道问题的自动化解决方案
7. Withdrawal: Optimization of Low-Thrust Gravity-Assist Trajectories via Optimality-Preserving Transformation [O] . Zhemin Chi, Gao Tang, Fanghua Jiang, 2020

机译：撤回：通过最优状态改变进行低推力重力辅助轨迹的优化
8. Time-Regularized Multiple Gravity-Assist Low-Thrust Bounded-Impulse Model for Trajectory Optimization. [R] . Ellison, D. H., Englander, J. A., Conway, B. A. 2017

机译：时间正则化多重力辅助低推力有界脉冲模型用于轨迹优化。

Optimization of the Transfer Trajectory of a Low-Thrust Spacecraft for Research of Jupiter Using an Earth Gravity-Assist Maneuver

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