Linearization Methods for Problems of Optimizing Low-Thrust Spacecraft Trajectories: Test Problem Solutions

Kazmerchuk P. V.

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Linearization Methods for Problems of Optimizing Low-Thrust Spacecraft Trajectories: Test Problem Solutions

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

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摘要

Several test problems are solved with the modified linearization method (MLM) demonstrating its features and possibilities.

机译：改进的线性化方法（MLM）展示了其功能和可能性，解决了一些测试问题。

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来源
《Solar system research》 |2018年第7期|649-654|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: Verification Procedure [J] . Kazmerchuk P. V. Solar system research . 2018,第7期

机译：低推力航天器轨迹优化问题的线性化方法：验证程序
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: Test Problem Solutions

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