Optimization of Interplanetary Flights of Spacecraft with Low-thrust Engines Taking into Account the Ellipticity and Noncoplanarity of Planetary Orbits

V. V. Salmin; O. L. Starinova

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Optimization of Interplanetary Flights of Spacecraft with Low-thrust Engines Taking into Account the Ellipticity and Noncoplanarity of Planetary Orbits

机译：考虑行星轨道的椭圆率和非共面性的低推力发动机航天器行星际飞行优化

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来源
《Космические исследования》 |2001年第1期|p.51-59|共9页
作者
V. V. Salmin; O. L. Starinova;
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正文语种 rus
中图分类航天（宇宙航行）;
关键词
planetary orbits; noncoplanarity; ellipticity; low thrust engines;

机译：行星轨道非共面性椭圆度低推力发动机;

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专利

1. Quasioptimal Control with Feedback for Multiorbit Low-Thrust Transfer between Noncoplanar Elliptic and Circular Orbits [J] . V. G. Petukhov Cosmic research . 2011,第2期

机译：非共面椭圆和圆形轨道之间多轨道低推力传递的带反馈的拟最优控制
2. Optimal Multi-Orbit Trajectories for Inserting a Low-Thrust Spacecraft to a High Elliptic Orbit [J] . V. G. Petukhov Cosmic research . 2009,第3期

机译：将低推力航天器插入高椭圆轨道的最优多轨道轨迹
3. Analysis of the Structure of Families of Locally Optimum Solutions to the Problem of the Interplanetary Transfer of a Spacecraft with a Low-Thrust Engine [J] . Vorobev A. L., Elnikov R. V. Cosmic research . 2018,第5期

机译：低推力发动机航天器行星际传递问题的局部最优解的族结构分析
4. Optimum program of control of continuous low-thrust at flight between noncoplanar elliptical and geostationary orbits [C] . Pavel V. Fadeenkov, Sergey A. Ishkov International Conference on Mathematical Problems in Engineering, Aerospace and Sciences . 2018

机译：在非平板椭圆形和地球静止轨道之间的飞行中连续低推力的最佳控制计划
5. AN OPTIMIZATION METHOD FOR THE PRELIMINARY DESIGN OF INTERPLANETARY AEROBRAKING MISSIONS (SPACECRAFT, ORBIT MECHANICS). [D] . HOFFMAN, STEPHEN JAMES. 1984

机译：行星际航空制动任务（空间工艺，轨道力学）的初步设计的一种优化方法。
6. A Submillimeter-Level Relative Navigation Technology for Spacecraft Formation Flying in Highly Elliptical Orbit [O] . Xiaoliang Wang, Deren Gong, Yifei Jiang, 2020

机译：高度椭圆轨道上飞船形成飞行的海底级相对导航技术
7. Multi-Step Optimization Strategy for Fuel-Optimal Orbital Transfer of Low-Thrust Spacecraft [O] . M. Rasotto, R. Armellin, P. Di Lizia 2016

机译：低推力航天器燃料最优轨道转移的多步优化策略
8. Start Solution for Interplanetary Low Thrust Trajectory Optimization and Model Refinement. Volume 3. Low Thrust Orbit Optimization for Interplanetary Missions Using a Pontryagin/Lambert Approach [R] . Hersom, S. E., Maany, Z. A. 1985

机译：行星际低推力轨迹优化和模型细化的启动解决方案。第3卷。使用pontryagin / Lambert方法进行行星际任务的低推力轨道优化

Optimization of Interplanetary Flights of Spacecraft with Low-thrust Engines Taking into Account the Ellipticity and Noncoplanarity of Planetary Orbits

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