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A SURVEY OF THE INFLUENCE OF VARIATIONS IN STAGE CHARACTERISTICS ON OPTIMIZED TRAJECTORY SHAPING. PART II- TRANSFER FROM CIRCULAR ORBITS INTO A SPACE FIXED ELLIPSE

机译：阶段特征变化对优化轨迹形状影响的调查。第二部分 - 从圆形轨道转移到空间固定椭圆机

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Optimum thrust to weight ratio for orbital transfer - circular to elliptical orbit

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作者
Mc Daniel, G.;
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年度 1963
页码 1-81
总页数 81
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
CIRCULAR ORBITS; ELLIPSES; ELLIPTICAL ORBITS; SURVEYS; THRUST PROGRAMMING; THRUST-WEIGHT RATIO; TRAJECTORIES; TRANSFER ORBITS; CIRCULAR ORBIT; ELLIPTICAL ORBIT; OPTIMUM THRUST PROGRAMMING; ORBITAL TRANSFER;

机译：圆形轨道;省略号;椭圆轨道;调查;推进程序设计;推力重量比;的轨迹;转移轨道;圆形轨道; ELLIpTICaL ORBIT;最优推动程序设计; ORBITaL TRaNsFER;

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专利

1. On Solving the Problems of Optimization of Trajectories of Many-Revolution Orbit Transfers of Spacecraft [J] . S. Yu. Ryzhov, I. S. Grigoriev Cosmic research . 2006,第3期

机译：解决航天器多次旋转轨道转移轨迹优化问题
2. Trajectory optimization of spacecraft high-thrust orbit transfer using a modified evolutionary algorithm [J] . Shirazi Abolfazl Engineering Optimization . 2016,第10a12期

机译：改进的进化算法优化航天器高推力轨道转移的轨迹
3. Optimization of Interorbital Three-dimensional Transfer Trajectories for Stage Spacecraft [J] . I. S. Grigorev, I. A. Danilina Automation and Remote Control . 2007,第8期

机译：级航天器轨道间三维转移轨迹的优化
4. Study on trajectory optimization for single-stage-to-orbit space planes using gauss pseudospectral method [C] . Ruizhi He, Peijun Zhang, Luhua Liu, Chinese Control and Decision Conference . 2017

机译：高斯伪谱法研究单阶段到轨道空间平面的轨迹优化
5. Trajectory optimization of low-thrust orbit transfers [D] . Graham, Kathryn Frances. 2015

机译：低推力轨道转移的轨迹优化
6. The Ascent Trajectory Optimization of Two-Stage-To-Orbit Aerospace Plane Based on Pseudospectral Method [O] . Song Jing, Su Haoqin 2015

机译：基于伪谱法的两轨制航天飞机上升轨迹优化
7. A SURVEY OF THE INFLUENCE OF VARIATIONS IN STAGE CHARACTERISTICS ON OPTIMIZED TRAJECTORY SHAPING. PART I- TWO STAGE VEHICLE INJECTION INTO CIRCULAR ORBITS [R] . Davidson, M. C., Jr. 1963

机译：阶段特征变化对优化轨迹形状影响的调查。第一部分 - 两个阶段的车辆注入圆形轨道

A SURVEY OF THE INFLUENCE OF VARIATIONS IN STAGE CHARACTERISTICS ON OPTIMIZED TRAJECTORY SHAPING. PART II- TRANSFER FROM CIRCULAR ORBITS INTO A SPACE FIXED ELLIPSE

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