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Orbital dynamics of 'Smart-Dust' devices with solar radiation pressure and drag

机译:具有太阳辐射压力和阻力的“智能尘埃”装置的轨道动力学

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摘要

This paper investigates how perturbations due to asymmetric solar radiation pressure, in the presence of Earth shadow, and atmospheric drag can be balanced to obtain long-lived Earth-centered orbits for swarms of microscale " smart-dust" devices, without the use of active control. The secular variation of Keplerian elements is expressed analytically through an averaging technique. Families of solutions are then identified in which sun-synchronous apse-line precession is achieved passively to maintain asymmetric solar radiation pressure. The long-term orbit evolution is characterized by librational motion, progressively decaying due to the nonconservative effect of atmospheric drag. Long-lived orbits can then be designed through the interaction of energy gain from asymmetric solar radiation pressure and energy dissipation due to drag. In this way, the usual short drag lifetime of such higharea- to-mass spacecraft can be greatly extended (and indeed selected). In addition, the effect of atmospheric drag can be exploited to ensure the rapid end-of-life decay of such devices, thus preventing long-lived orbit debris. © 2011 by Camilla Colombo and Colin McInnes. Published by the American Institute of Aeronautics and Astronautics, Inc.
机译:本文研究了在存在地球阴影和大气阻力的情况下,如何平衡由不对称的太阳辐射压力引起的扰动,以在不使用有源“微尘”设备的情况下获得长寿命的以地球为中心的轨道。控制。开普勒元素的长期变化是通过平均技术来分析表示的。然后确定一系列解决方案,在这些解决方案中,被动地实现了与太阳同步的近地点线的进动,以维持不对称的太阳辐射压力。长期轨道演化的特征是自由运动,由于大气阻力的非保守作用而逐渐衰减。然后可以通过不对称太阳辐射压力的能量增益与阻力引起的能量耗散的相互作用来设计长寿命轨道。这样,这种大面积质量的航天器通常的短拖曳寿命就可以大大延长(并且确实可以选择)。另外,可以利用大气阻力的作用来确保这种装置的寿命终止快速衰减,从而防止长寿命的轨道碎片。 ©2011卡米拉·科伦坡和科林·麦金尼斯。由美国航空航天学会出版。

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