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Dynamics of a partial space elevator with multiple climbers

机译:具有多个爬升器的部分空间电梯的动力学

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摘要

A space elevator has been proposed as an alternate method for space transportation. The materials currently in existence are not strong enough to support the stresses generated in a full structure; the use of a partial elevator may be considered instead, at least for the near term. For a sufficiently long ribbon/tether floating in space, a payload can dock at its lower end, use a climber to ascend to higher altitudes and then be launched, thereby saving in fuel consumption. Since this structure can be modelled as a multiple-body system with a very long tether, the dynamics of such a system is studied in this paper. In the first part, the equations of motion are derived using the Lagrangian approach, and then linearized in order to determine the libration frequencies. In the case where a single climber is in use, the governing equations are solved numerically; it is noted that the motion of the climber introduces oscillations in the tether, thus introducing errors into the desired orbit of the payload. In the second part, the use of multiple climbers is investigated in an attempt to minimize these errors.
机译:已经提出了太空升降机作为用于太空运输的替代方法。当前存在的材料强度不足以承受整个结构中产生的应力。至少在短期内,可以考虑使用部分电梯。对于在太空中漂浮的足够长的色带/绳索,有效载荷可以停靠在其下端,使用登山者登高至更高的高度,然后再下山,从而节省了燃油消耗。由于此结构可以建模为具有很长系链的多体系统,因此本文研究了这种系统的动力学。在第一部分中,使用拉格朗日方法导出了运动方程,然后对其进行线性化以确定自由频率。在使用单个登山器的情况下,控制方程通过数值求解;注意,爬升器的运动在系绳中引入了振动,从而将误差引入了有效载荷的期望轨道。在第二部分中,研究了使用多个攀登机的尝试,以尽量减少这些错误。

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