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Equilibrium Positions of a Cable-Connected Satellites System under Several Influences

机译:几种影响下的有线卫星系统的平衡位置

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The present paper deals with the study of equilibrium positions of the motion of a system of two artificial satellites connected by a light, flexible, inextensible and non-conducting cable under the influence of solar radiation pressure, earth’s oblateness, shadow of the earth and air resistance. Here, we study the case of circular orbit of the centre of mass of the system. We derive differential equations of motion of the system. General solutions of the differential equations are beyond the reach. On the other hand, the general solutions do not serve our purpose. Jacobian integral of the system has also been obtained. Thereafter equilibrium positions of the motion of the system have been obtained.
机译:本文研究在太阳辐射压力,地球扁率,地球和空气阴影的影响下,由两根人造卫星组成的系统的运动平衡位置,该人造卫星由轻,柔性,不可扩展且不导电的电缆连接抵抗性。在这里,我们研究系统质心的圆形轨道的情况。我们得出系统运动的微分方程。微分方程的一般解超出了范围。另一方面,一般解决方案不符合我们的目的。还获得了系统的雅可比积分。此后,已经获得系统运动的平衡位置。

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