Linearization Methods for Problems of Optimizing Low-Thrust Spacecraft Trajectories: Verification Procedure

Kazmerchuk P. V.

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Linearization Methods for Problems of Optimizing Low-Thrust Spacecraft Trajectories: Verification Procedure

机译：低推力航天器轨迹优化问题的线性化方法：验证程序

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摘要

Several well-studied problems for optimizing low-thrust spacecraft trajectories are solved using the modified linearization method (MLM). The results are compared with the results obtained by other authors. On this basis, conclusions are drawn on the possible use of the modified linearization method for optimizing low-thrust spacecraft trajectories.

机译：使用改进的线性化方法（MLM）解决了一些针对低推力航天器轨迹进行优化研究的问题。将结果与其他作者获得的结果进行比较。在此基础上，得出结论：可能使用改进的线性化方法来优化低推力航天器的轨迹。

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来源
《Solar system research》 |2018年第7期|630-635|共6页
作者
Kazmerchuk P. V.;
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作者单位

Lavochkin Assoc, Chimki, 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
linearization method; low thrust; nonlinear optimization;

机译：线性化方法低推力非线性优化;

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专利

1. Linearization Methods for Problems of Optimizing Low-Thrust Spacecraft Trajectories: Test Problem Solutions [J] . Kazmerchuk P. V. Solar system research . 2018,第7期

机译：优化低推力航天器轨迹问题的线性化方法：测试问题解决方案
2. Comparison of the Legendre-Gauss pseudospectral and Hermite-Legendre-Gauss-Lobatto methods for low-thrust spacecraft trajectory optimization [J] . Sanjeev Narayanaswamy, Christopher J. Damaren Aerospace Systems . 2020,第1期

机译：Legendre-Gauss伪谱与Hermite-Legendre-Gauss-Lobatto方法用于低推力航天器轨迹优化的比较
3. Low-thrust spacecraft trajectory optimization via a DNN-based method [J] . Shanshan Yin, Jian Li, Lin Cheng Advances in space research . 2020,第7期

机译：通过基于DNN的方法的低推力航天器轨迹优化
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. Optimization of low-thrust spacecraft trajectories by direct shooting methods. [D] . Rampersad, Christopher. 2004

机译：通过直接射击方法优化低推力航天器的轨迹。
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. Evolutionary neurocontrol: A novel method for low-thrust gravity-assist trajectory optimization [O] . Carnelli, L., Dachwald, Bernd, Vasile, Massimiliano 2009

机译：进化神经控制：一种低推力重力辅助轨迹优化的新方法

Linearization Methods for Problems of Optimizing Low-Thrust Spacecraft Trajectories: Verification Procedure

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