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TWO-CRAFT COULOMB FORMATION RELATIVE EQUILIBRIA ABOUT CIRCULAR ORBITS AND LIBRATION POINTS

机译:关于圆轨道和交点的两工艺库仑形成相对平衡

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The charged relative equilibria of a two spacecraft Coulomb formation moving in the contextof a restricted two-body system and a circularly restricted three-body system are investigated.For a two-spacecraft formation moving in a central gravitational field it is oftenassumed that the center of the circular orbit is located at the primary mass, and the centerof mass of the formation orbits around the primary in a great circle orbit. The relative equilibriumis called great circle if the center of mass of the formation moves on the plane withthe center of the gravitational field residing on it; otherwise, it is called a non-great-circleorbit. Previous research shows that non-great-circle equilibria in low Earth orbits, have adeflection from the great circle equilibria of about a degree when spacecraft with unequalmasses are separated by 350 km. This paper investigates these equilibria (radial, tangentialand orbit normal in circular Earth orbit and Earth-Moon Libration points) in the context oftwo spacecraft Coulomb formation, and shows that the equilibria deflections are negligible(on the order of 10?6 degrees) even for very heterogeneous mass distributions. Further, thenon-great-circle equilibria conditions for a two-spacecraft virtual Coulomb structure at theLagrangian Libration points are developed. The development is based on exact gravitationaland Coulomb potentials and considers the effect of mass asymmetry of the formation in theproblem formulation.
机译:在上下文中移动的两个航天器库仑编队的带电相对平衡 研究了约束两体系统和圆形约束三体系统的结构。 对于在中央引力场中移动的两航天器编队来说,通常是 假设圆轨道的中心位于主要质量,并且中心 在一个大的圆形轨道中围绕主轨道的编队轨道的质量。相对平衡 如果地层的质心在平面上移动,则称为大圆 重力场的中心;否则,称为非大圆 轨道。先前的研究表明,低地球轨道上的非大圆平衡具有 当航天器不等时偏离大圆平衡约一个度 群众相距350公里。本文研究了这些平衡(径向,切向 在圆形地球轨道和月球地球交汇点处的轨道法线和轨道法线) 两个航天器的库仑形成,并表明平衡偏差可忽略不计 (大约10?6度)甚至对于非常不均匀的质量分布。此外, 两航天器虚拟库仑结构的非大圆平衡条件。 拉格朗日图书馆的发展点。该开发基于精确的引力 和库仑势,并考虑了地层中质量不对称的影响 问题表述。

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