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Optimum Two-Pulse Passage Between Orbits with Small Inclinations and Eccentricities

机译：具有小倾角和偏心的轨道之间的最佳双脉冲通道

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摘要

An analytical formulation is given of the trajectory of an optimum two-pulse flight between orbits with small inclinations and eccentricities. (Author)

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Novoselov, V. S.;
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年度 1965
页码 p.1-2
总页数 2
原文格式 PDF
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Space flight ; Interplanetary trajectories ; Optimization ; Calculus of variations ; Celestial mechanics ; Transfer trajectories ; USSR;

机译：太空飞行;行星际轨迹;优化;变分微积分;天体力学;转移轨迹;苏联;

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专利

1. Frozen orbits at high eccentricity and inclination: Application to Mercury orbiter [J] . Delsate N., Robutel P., Lema?tre A., Celestial Mechanics and Dynamical Astronomy: An international journal of space dynamics . 2010,第3期

机译：高偏心率和倾斜度的冻结轨道：在水银轨道器上的应用
2. Frozen orbits at high eccentricity and inclination: application to Mercury orbiter [J] . N. Delsate, P. Robutel, A. Lemaître, Celestial Mechanics and Dynamical Astronomy . 2010,第3期

机译：高偏心率和倾斜度的冻结轨道：在水星轨道上的应用
3. Efficient onboard image motion compensation for orbital inclination and eccentricity of geostationary weather satellites [J] . Ramachandran M. P., Agarwal M. K., Daniel D. A. Proceedings of the Institution of Mechanical Engineers . 2020,第7期

机译：高效的轨道倾向和地球静止天气卫星偏心的车载运动补偿
4. High Velocity Aero-gravity Assist Applied on Eccentricity to Inclination Conversion for Reaching Solar Polar Orbit [C] . Tiago Monteiro Padovan, Yuki Kubo, Junichiro Kawaguchi, AIAA SciTech Forum and Exposition . 2020

机译：高速重力辅助在偏心度到倾角转换中的应用，以达到太阳极轨道
5. Sequential Estimation of Spacecraft Relative Orbits: Improving Observability with Nonlinearities, Chief Eccentricity, and Consensus Feedback [D] . Wang, Jingwei. 2018

机译：航天器相对轨道的顺序估计：通过非线性，主要偏心率和共识反馈提高可观察性
6. Colloquium Paper: Spectrum of 100-kyr glacial cycle: Orbital inclination not eccentricity [O] . Richard A. Muller, Gordon J. MacDonald 1997

机译：座谈会论文：100 kyr冰河周期的光谱：轨道倾角不偏心
7. Investigation of the Secular Acceleration of the Moon's Mean Motion, caused by the Secular Change in the Eccentricity of the Earth's Orbit; taking into Account Terms of the Order of m4, but neglecting the Eccentricity and Inclination of the Moon's Orbit [O] . J. C. Adams 1880

机译：由地球轨道偏心的世俗变化引起的月球平均运动的世俗加速调查;考虑到M4的顺序条款，但忽略了月球轨道的偏心和倾向
8. Numerical Determination of the Location of Critical Inclinations for Long Term High Eccentricity Orbits About Mars [R] . Durand, D. F. 1989

机译：火星长期高偏心轨道临界倾角位置的数值确定

Optimum Two-Pulse Passage Between Orbits with Small Inclinations and Eccentricities

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