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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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天体运动的三维DDA模拟
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作者 汪雨璇 喻勇 《长春师范大学学报》 2024年第8期46-53,共8页
不连续变形分析(DDA)方法广泛应用于岩土工程领域,其中三维球颗粒DDA(3D-SDDA)理论能够对球形物体模型的运动进行数值模拟。本研究将不连续变形分析方法应用于太阳系天体运行模拟,将各天体看作球状物体,仅考虑天体间的引力和其自身惯性... 不连续变形分析(DDA)方法广泛应用于岩土工程领域,其中三维球颗粒DDA(3D-SDDA)理论能够对球形物体模型的运动进行数值模拟。本研究将不连续变形分析方法应用于太阳系天体运行模拟,将各天体看作球状物体,仅考虑天体间的引力和其自身惯性力,通过建立系统总体平衡方程式,推导载荷矩阵方程,求解总体方程,编写Matlab计算程序,从而得到各天体的运动参数,对天体运动进行数值模拟。结果表明,利用3D-SDDA理论能够模拟日-地二体系统和日-地-月三体系统在宇宙空间中的运行状态,获取任意时刻天体的空间位置和速度信息。分别将日-地二体系统的数值计算结果与开普勒计算方法所得结果对比,日-地-月三体系统的结果与虚拟天文馆软件Stellarium高精度数据对比,结果吻合良好。同时输入月全食发生的限制条件,能够正确预测出月全食发生时刻。 展开更多
关键词 DDA 天体运行 数值模拟 日-地系统 日-地-月系统
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Everything Is a Circle: A New Universal Orbital Model
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作者 Asli Pinar Tan 《Advances in Aerospace Science and Technology》 2024年第3期94-116,共23页
Based on measured astronomical position data of heavenly objects in the Solar System and other planetary systems, all bodies in space seem to move in some kind of elliptical motion with respect to each other. Accordin... Based on measured astronomical position data of heavenly objects in the Solar System and other planetary systems, all bodies in space seem to move in some kind of elliptical motion with respect to each other. According to Kepler’s 1st Law, “orbit of a planet with respect to the Sun is an ellipse, with the Sun at one of the two foci.” Orbit of the Moon with respect to Earth is also distinctly elliptical, but this ellipse has a varying eccentricity as the Moon comes closer to and goes farther away from the Earth in a harmonic style along a full cycle of this ellipse. In this paper, our research results are summarized, where it is first mathematically shown that the “distance between points around any two different circles in three-dimensional space” is equivalent to the “distance of points around a vector ellipse to another fixed or moving point, as in two-dimensional space”. What is done is equivalent to showing that bodies moving on two different circular orbits in space vector-wise behave as if moving on an elliptical path with respect to each other, and virtually seeing each other as positioned at an instantaneously stationary point in space on their relative ecliptic plane, whether they are moving with the same angular velocity, or different but fixed angular velocities, or even with different and changing angular velocities with respect to their own centers of revolution. This mathematical revelation has the potential to lead to far reaching discoveries in physics, enabling more insight into forces of nature, with a formulation of a new fundamental model regarding the motions of bodies in the Universe, including the Sun, Planets, and Satellites in the Solar System and elsewhere, as well as at particle and subatomic level. Based on the demonstrated mathematical analysis, as they exhibit almost fixed elliptic orbits relative to one another over time, the assertion is made that the Sun, the Earth, and the Moon must each be revolving in their individual circular orbits of revolution in space. With this expectation, individual orbital parameters of the Sun, the Earth, and the Moon are calculated based on observed Earth to Sun and Earth to Moon distance data, also using analytical methods developed as part of this research to an approximation. This calculation and analysis process have revealed additional results aligned with observation, and this also supports our assertion that the Sun, the Earth, and the Moon must actually be revolving in individual circular orbits. 展开更多
关键词 Solar System Planetary System PLANET Satellite Earth MOON Topology Circle Sun ELLIPSE ORBIT TRAJECTORY Orbital Mechanics
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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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