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Start Solution for Interplanetary Low Thrust Trajectory Optimisation and Model Refinement. Volume 2. User's Guide to the Software for Low Thrust Orbit Optimization for Interplanetary Missions Using a Linear Model

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2卷。使用线性模型的行星际任务低推力轨道优化软件用户指南

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摘要

A user guide for a low thrust orbit control problem is presented.

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作者
Hersom, S. E.; Maany, Z. A.; Patel, K. D.;
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年度 1984
页码 p.1-66
总页数 66
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Interplanetary trajectories; Trajectory optimization; Low thrust; User manuals (Computer programs); Asteroid missions; Fortran; Orbital mechanics; Satellite orbits;

机译：行星际轨迹;轨迹优化;低推力;用户手册（计算机程序）;小行星任务; Fortran;轨道力学;卫星轨道;

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专利

1. Simple Semi-Analytic Model for Optimized Interplanetary Low-Thrust Trajectories Using Solar Electric Propulsion [J] . David Y. Oh, Damon Landau Journal of Spacecraft and Rockets . 2013,第3期

机译：利用太阳推进力优化行星际低推力轨迹的简单半解析模型
2. Multi-Objective Low-Thrust Interplanetary Trajectory Optimization Based on Generalized Logarithmic Spirals [J] . Morante David, Sanjurjo Rivo Manuel, Soler Manuel Journal of guidance, control, and dynamics . 2019,第3期

机译：基于广义对数螺旋的多目标低推力行星际轨迹优化
3. Technique of Optimizing Trajectories of Interplanetary Transfers with Gravity Assisted Maneuvers Using Low-Thrust Propulsion [J] . Orlov A. A. Cosmic research . 2019,第5期

机译：低推力重力辅助机动优化行星际转移轨迹的技术
4. Low- Thrust Interplanetary Orbit Transfers Using Hybrid Trajectory Optimization Method with Multiple Shooting [C] . Y. Gao, C. Kluever AIAA Guidance, Navigation, and Control Conference ; 22nd Applied Aerodynamics Conference and Exhibit ; AIAA/AAS Astrodynamics Specialist Conference and Exhibit . 2004

机译：低空推力行星际轨道多发射混合轨迹优化方法
5. Automated trajectory design for impulsive and low thrust interplanetary mission analysis. [D] . Wagner, Samuel Arthur. 2014

机译：脉冲和低推力行星际任务分析的自动轨迹设计。
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. Automated trajectory design for impulsive and low thrust interplanetary mission analysis [O] . Wagner Samuel Arthur 2014

机译：脉冲和低推力行星际任务分析的自动轨迹设计
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

Start Solution for Interplanetary Low Thrust Trajectory Optimisation and Model Refinement. Volume 2. User's Guide to the Software for Low Thrust Orbit Optimization for Interplanetary Missions Using a Linear Model

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