Space debris selection and optimal guidance for removal in the SSO with low-thrust propulsion

J.T. Olympio; N. Frouvelle

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Space debris selection and optimal guidance for removal in the SSO with low-thrust propulsion

机译：低推力的空间碎片选择和SSO去除的最佳指导

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The current paper deals with the mission design of a generic active space debris removal spacecraft. Considered space debris are all on sun-synchronous orbits. A perturbed Lambert's problem, modelling the transfer between two space debris is devised to take into account J_2 perturbation, and to quickly evaluate mission scenarios. A robust approach, using techniques of global optimisation, is followed to find the optimal space debris sequence and mission strategy. Low-thrust optimisation is then performed to turn bi-impulse transfers into optimal low-thrust transfers, and refine the selected scenarios.

机译：目前的论文涉及通用主动空间碎片清除航天器的任务设计。被认为是空间碎片的都是太阳同步轨道。设计了一个扰动的兰伯特问题，对两个空间碎片之间的传递进行建模，以考虑到J_2扰动，并快速评估任务场景。遵循使用全局优化技术的可靠方法，以找到最佳的空间碎片序列和任务策略。然后执行低推力优化，以将双脉冲传递转换为最佳的低推力传递，并优化所选方案。

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来源
《Acta astronautica》 |2014年第junaajula期|263-275|共13页
作者
J.T. Olympio; N. Frouvelle;
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作者单位

CS Communication et Systeme, 5 rue Brindejonc des Moulinais, BP 15872, 31506 Toulouse Cedex 5, France;

CS Communication et Systeme, 5 rue Brindejonc des Moulinais, BP 15872, 31506 Toulouse Cedex 5, France;

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收录信息美国《科学引文索引》(SCI);美国《工程索引》(EI);
原文格式 PDF
正文语种 eng
中图分类
关键词
Space debris; Sun-synchronous orbit; Low-thrust propulsion; Optimisation; Optimal control;

机译：空间碎片;太阳同步轨道;低推力推进;优化;最佳控制;

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专利

1. Optimal planning for a multiple space debris removal mission using high-accuracy low-thrust transfers [J] . Jorgensen Mikkel K., Sharf Inna Acta astronautica . 2020,第Jula期

机译：使用高精度低推力转移的多个空间碎片去除任务的最佳规划
2. Real Time Optimal Guidance of Low-Thrust Spacecraft: An Application of Nonlinear Model Predictive Control [J] . JUAN JOSE ARRIETA-CAMACHO, LORENZ T. BIEGLER Annals of the New York Academy of Sciences . 2005,第Dec期

机译：低推力航天器实时最优制导：非线性模型预测控制的应用
3. Small Electric Propulsion Platform for Active Space Debris Removal [J] . Ruggiero A., Pergola P., Andrenucci M. Plasma Science, IEEE Transactions on . 2015,第12期

机译：小型电动推进平台，用于主动空间杂物清除
4. DEBRIS SELECTION AND OPTIMAL PATH PLANNING FOR DEBRIS REMOVAL ON THE SSO: IMPULSIVE-THRUST OPTION [C] . J. T. Olympio, N. Frouvelle 6th European Conference on Space Debris . 2013

机译：在SSO上进行碎片清除的碎片选择和最佳路径规划：冲动式推力选择
5. Guidance of low-thrust spacecraft. [D] . Huang, Rosemary Chia-Hua. 2012

机译：低推力航天器的指导。
6. Space Debris Removal: Learning to Cooperate and the Price of Anarchy [O] . Richard Klima, Daan Bloembergen, Rahul Savani, 2018

机译：拆除空间碎片：学习合作和无政府状态的价格
7. Optimal guidance of low-thrust interplanetary space vehicles [O] . Ash Gerald R. 1969

机译：低推力行星际航天器的最佳制导
8. RS-34 Phoenix In-Space Propulsion System Applied to Active Debris Removal Mission. [R] . Esther, E. A., Burnside, C. G., Capizzo, P. D., 2014

机译：Rs-34 phoenix太空推进系统应用于主动碎屑清除任务。

Space debris selection and optimal guidance for removal in the SSO with low-thrust propulsion

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