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Solution set on the natural satellite formation orbits under first-order earth's non-spherical perturbation 被引量:1
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作者 Humei Wang Wei Yang Junfeng Li 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2005年第5期503-510,共8页
Using the reference orbital element approach, the precise governing equations for the relative motion of formation flight are formulated. A number of ideal formations with respect to an elliptic orbit can be designed ... Using the reference orbital element approach, the precise governing equations for the relative motion of formation flight are formulated. A number of ideal formations with respect to an elliptic orbit can be designed based on the relative motion analysis from the equations. The features of the oscillating reference orbital elements are studied by using the perturbation theory. The changes in the relative orbit under perturbation are divided into three categories, termed scale enlargement, drift and distortion respectively. By properly choosing the initial mean orbital elements for the leader and follower satellites, the deviations from originally regular formation orbit caused by the perturbation can be suppressed. Thereby the natural formation is set up. It behaves either like non-disturbed or need little control to maintain. The presented reference orbital element approach highlights the kinematics properties of the relative motion and is convenient to incorporate the results of perturbation analysis on orbital elements. This method of formation design has advantages over other methods in seeking natural formation and in initializing formation. 展开更多
关键词 orbital mechanics . Satellite formation flight .orbital elements . Reference orbital elements . perturbation
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Updating the Historical Perspective of the Interaction of Gravitational Field and Orbit in Sun-Planet-Moon System
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作者 Yin Zhu 《International Journal of Astronomy and Astrophysics》 2021年第3期343-369,共27页
Studying the two famous old problems that why the moon can move around the Sun and why the orbit of the Moon around the Earth cannot be broken off by the Sun under the condition calculating with <em>F</em>... Studying the two famous old problems that why the moon can move around the Sun and why the orbit of the Moon around the Earth cannot be broken off by the Sun under the condition calculating with <em>F</em>=<em>GMm</em>/<em>R</em><sup>2</sup>, the attractive force of the Sun on the Moon is almost 2.2 times that of the Earth, we found that the planet and moon are unified as one single gravitational unit which results in that the Sun cannot have the force of <em style="white-space:normal;">F</em><span style="white-space:normal;">=</span><em style="white-space:normal;">GMm</em><span style="white-space:normal;">/</span><em style="white-space:normal;">R</em><sup style="white-space:normal;">2</sup> on the moon. The moon is moved by the gravitational unit orbiting around the Sun. It could indicate that the gravitational field of the moon is limited inside the unit and the gravitational fields of both the planet and moon are unified as one single field interacting with the Sun. The findings are further clarified by reestablishing Newton’s repulsive gravity. 展开更多
关键词 Interaction of Gravitational Field Three-Body Problem orbital perturbation Theory Repulsive Gravity Neutralization of Gravity
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