Finding Best Solution in Low-Thrust Trajectory Optimization by Two-Phase Homotopy

Pan Binfeng; Pan Xun; Lu Ping

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Finding Best Solution in Low-Thrust Trajectory Optimization by Two-Phase Homotopy

机译：两相同伦寻找低推力轨迹优化的最佳解决方案

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来源
《Journal of Spacecraft and Rockets》 |2019年第1期|283-291|共9页
作者
Pan Binfeng; Pan Xun; Lu Ping;
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作者单位

Northwestern Polytech Univ, Coll Astronaut, Xian 710072, Shaanxi, Peoples R China;

Northwestern Polytech Univ, Coll Astronaut, Xian 710072, Shaanxi, Peoples R China;

San Diego State Univ, Dept Aerosp Engn, San Diego, CA 92182 USA;

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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
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1. Homotopy method for optimization of variable-specific-impulse low-thrust trajectories [J] . Chi Zhemin, Yang Hongwei, Chen Shiyu, Astrophysics and space science . 2017,第11期

机译：用于优化可变特定脉冲低推力轨迹的同型方法
2. 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
3. A quadratic homotopy method for fuel-optimal low-thrust trajectory design [J] . Pan Binfeng, Pan Xun, Ma Yangyang Proceedings of the Institution of Mechanical Engineers . 2019,第5期

机译：燃料最优低推力轨迹设计的二次同伦方法
4. Homotopy Method for Finding the Global Solution of Post-contingency Optimal Power Flow [C] . SangWoo Park, Elizabeth Glista, Javad Lavaei, Annual American Control Conference . 2020

机译：事后最优潮流全局解的同伦方法
5. Low-thrust Trajectory Optimization in the Circular Restricted Three Body Problem [D] . Chikine, Saikiran. 2019

机译：循环限制的三个身体问题中的低推力轨迹优化
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. Low-Thrust Trajectory Optimization with Simplified SQP Algorithm. [R] . Parrish, N. L., Scheeres, D. J. 2017

机译：基于简化sQp算法的低推力轨迹优化。

Finding Best Solution in Low-Thrust Trajectory Optimization by Two-Phase Homotopy

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