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Optimization of transfer schemes between passive space objects in GEO vicinity

机译:Geo附近被动空间对象之间传输方案的优化

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The paper compares two variants of re-orbiting space debris objects from the geosynchronous (GEO) region. Under the first reorbiting variant, a spacecraft-collector (SC-collector) transfers between target objects (87 upper stages). A re-orbiting of the next in line object into a disposal orbit (DO) is carried out using special kits (thruster de-orbiting kits, TDK) which are placed on space debris objects by the SC-collector. Under the second variant, the object is pushed to a DO by the SC-collector itself, which then moves to a new space debris object from the DO of the previous object. It is shown that due to slow evolution of the orbital parameters in the GEO region, the same transfer schemes can be used for both re-orbiting variants. We describe geometrical peculiarities of relative positions of orbits in the near-equatorial region and consider two transfer schemes between objects. Under the first scheme, a transfer is executed when the orbits have the same inclination near the equator, and under the second scheme, when the orbit of the next object has the smallest inclination. Calculations show that both schemes are practically equivalent in terms of the averaged specific losses of the summary characteristic velocity (SCV) for a transfer (between two objects) and the duration -- however, not all objects under consideration can be covered under the first scheme (when transfers are executed at times of equal inclinations). Hence, priority should be given to the scheme when the transfers are executed when the orbital inclination of the next object attains its smallest value. Based on the results of calculations, a conclusion can be made that 6 SC-collectors are required to clean the GEO protected region from spent upper stages. The active service life of each active SC is expected to be at most 8 years and its required SCV budget is at most 0.7 km/sec. A re-orbiting of one object to a DO requires on the average 10 m/sec; the return to a new object from the DO of th
机译:本文比较了来自地球同步(地理)区域的再轨道空间碎屑物体的两个变体。在第一再吸收变型下,航天器 - 集电体(SC-Collector)在目标物体(87个上阶段)之间转移。将下一个线对象的重新轨道在处理轨道(DO)中使用SC-Collector放置在空间碎屑物体上的特殊套件(推进器去轨道,TDK)进行。在第二变型下,对象被SC-Collector本身推送到DO,然后从先前对象的DO移动到新的空间碎片对象。结果表明,由于地理区域中的轨道参数的慢速演化,相同的转移方案可用于重新轨道变体。我们描述近赤道区域中轨道相对位置的几何特性,并考虑物体之间的两个转移方案。在第一种方案下,当轨道在赤道附近具有相同的倾斜度并且在第二方案下,当下一个对象的轨道具有最小倾斜时,执行传送。计算表明,两种方案都在实际上等同于概述特征速度(SCV)的平均特定损失,用于转移(在两个物体之间)和持续时间之间 - 但是,并非所有正在考虑的对象都可以在第一个方案下涵盖(当在等倾斜时执行转移时)。因此,当下一个对象的轨道倾斜度达到其最小值时执行转移时,应优先考虑该方案。基于计算结果,可以结论,需要6个SC收集器来清除从花费上阶段的地理保护区。每个活动SC的主动使用寿命预计最多为8年,其必需的SCV预算最多为0.7公里/秒。将一个对象的重新轨道对待一个对象需要平均10米/秒;从do返回新对象

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