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Design of low-energy transfer from lunar orbit to asteroid in the Sun-Earth-Moon system
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作者 Ya-Min Wang Dong Qiao Ping-Yuan Cui 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2014年第6期966-972,共7页
Asteroid exploration trajectories which start from a lunar orbit are investigated in this work.It is assumed that the probe departs from lunar orbit and returns to the vicinity of Earth,then escapes from the Earth by ... Asteroid exploration trajectories which start from a lunar orbit are investigated in this work.It is assumed that the probe departs from lunar orbit and returns to the vicinity of Earth,then escapes from the Earth by performing a perigee maneuver.A low-energy transfer in Sun-EarthMoon system is adopted.First,the feasible region of lowenergy transfer from lunar orbit to perigee within 5 000 km height above the Earth surface in Sun-Earth-Moon system is calculated and analyzed.Three transfer types are found,i.e.,large maneuver and fast transfers,small maneuver and fast transfers,and disordered and slow transfers.Most of feasibility trajectories belong to the first two types.Then,the lowenergy trajectory leg from lunar orbit to perigee and a heliocentric trajectory leg from perigee to asteroid are patched by a perigee maneuver.The optimal full-transfer trajectory is obtained by exploiting the differential evolution algorithm.Finally,taking 4179 Toutatis asteroid as the target,some low-energy transfer trajectories are obtained and analyzed. 展开更多
关键词 Lunar orbit Asteroid exploration Low-energy transfer sun-earth-moon system
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Dark Galaxies, Sun-Earth-Moon Interaction, Tunguska Event—Explained by WUM
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作者 Vladimir S. Netchitailo 《Journal of High Energy Physics, Gravitation and Cosmology》 CAS 2024年第2期836-853,共18页
Great experimental results and observations achieved by Astronomy in the last decades revealed new unexplainable phenomena. Astronomers have conclusive new evidence that a recently discovered “dark galaxy” is, in fa... Great experimental results and observations achieved by Astronomy in the last decades revealed new unexplainable phenomena. Astronomers have conclusive new evidence that a recently discovered “dark galaxy” is, in fact, an object the size of a galaxy, made entirely of dark matter. They found that the speed of the Earth’s rotation varies randomly each day. 115 years ago, the Tunguska Event was observed, and astronomers still do not have an explanation of It. Main results of the present article are: 1) Dark galaxies explained by the spinning of their Dark Matter Cores with the surface speed at equator less than the escape velocity. Their Rotational Fission is not happening. Extrasolar systems do not emerge;2) 21-cm Emission explained by the self-annihilation of Dark Matter particles XIONs (5.3 μeV);3) Sun-Earth-Moon Interaction explained by the influence of the Sun’s and the Moon’s magnetic field on the electrical currents of the charged Geomagma (the 660-km layer), and, as a result, the Earth’s daylength varies;4) Tunguska Event explained by a huge atmospheric explosion of the Superbolide, which was a stable Dark Matter Bubble before entering the Earth’s atmosphere. 展开更多
关键词 World-Universe Model Dark Stars Dark Galaxies 21-cm Emission Formation of Macrostructures sun-earth-moon Interaction Tunguska Event Dark Matter
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基于日地月方位信息的自主导航系统的脉冲仿真和方位确定
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作者 荆武兴 李茂登 黄翔宇 《航天控制》 CSCD 北大核心 2011年第3期69-74,79,共7页
基于日地月信息的自主导航系统利用日地和月地夹角信息来确定卫星的轨道和姿态,具有很强的应用背景。它利用在轨的集成敏感器来敏感太阳、月球和地平边缘,从而产生相应的脉冲。利用脉冲的信息就可以确定日、地、月的方位信息,并可以确... 基于日地月信息的自主导航系统利用日地和月地夹角信息来确定卫星的轨道和姿态,具有很强的应用背景。它利用在轨的集成敏感器来敏感太阳、月球和地平边缘,从而产生相应的脉冲。利用脉冲的信息就可以确定日、地、月的方位信息,并可以确定日地和月地夹角。本文研究了该类自主导航系统的基于球形地球假设的方位确定算法,导航敏感器基于地球扁率的地平脉冲、太阳脉冲和月球脉冲的产生机制,并评估了地球扁率对方位确定的影响。仿真结果表明,如果脉冲产生机制中不考虑地球扁率,由脉冲计算出的月地夹角、日地夹角的精度能达到(10-10)°。如果脉冲机制中考虑地球扁率,而方位确定中不进行修正,由脉冲计算出的月(日)地夹角与真实的月(日)地夹角的最大误差有(0.12)°。 展开更多
关键词 自主导航系统 日地月方位信息 地球扁率 脉冲仿真
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准双椭圆三体模型
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作者 齐毅 徐世杰 《中国科学:物理学、力学、天文学》 CSCD 北大核心 2020年第7期98-107,共10页
本文我们提出了日地月准双椭圆三体问题(Quasi-Bielliptic Problem,QBEP)模型.该模型假设月球绕地球的轨道为受太阳引力摄动影响的准椭圆轨道,而地月质心绕太阳的轨道为严格的椭圆.此外我们认为日地月三个天体运行在同一轨道平面内.我... 本文我们提出了日地月准双椭圆三体问题(Quasi-Bielliptic Problem,QBEP)模型.该模型假设月球绕地球的轨道为受太阳引力摄动影响的准椭圆轨道,而地月质心绕太阳的轨道为严格的椭圆.此外我们认为日地月三个天体运行在同一轨道平面内.我们推导了月球准椭圆轨道的一阶展开解析表达式需要满足的微分方程,并利用我们提出的计算方法,将微分方程问题转化为线性方程组问题来进行求解.通过比较数值积分结果,我们方法的有效性得到了验证.而后我们详细比较了该解析结果与准双圆模型的差异,同时讨论了两个基准椭圆轨道偏心率对解析结果的影响. 展开更多
关键词 限制性四体问题 准双椭圆模型 日地月系统
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