首页> 外文会议>Symposium of the International Academy of Astronautics, Oct 2-6, 2000, Rio de Janeiro, Brazil >SELF-INDUCED COLLISION HAZARD IN HIGH AND MODERATE INCLINATION SATELLITE CONSTELLATIONS
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SELF-INDUCED COLLISION HAZARD IN HIGH AND MODERATE INCLINATION SATELLITE CONSTELLATIONS

机译:中高倾角卫星星座中的自激碰撞危险

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The assessment of the hazard posed by space debris to constellations of satellites in low Earth orbit is of growing importance, with the proliferation of proposed and implemented constellation systems with a variety of mission objectives. This applies to current constellation-based commercial communication systems, in particular, since these are typically deployed at altitudes where there is a peak in the space debris environment. An impact risk analysis is performed over a period of up to 1 month after a breakup event using two examples of constellation configurations. The first is similar to the IRIDIUM system, containing around 70 satellites in near-polar orbits at approximately 800 km altitude, and the second is a Globalstar-like configuration with 56 satellites at around 1400 km altitude, distributed in orbit planes inclined at 52°. The analysis is performed using the SDS software, which applies the probabilistic continuum dynamics technique. This has the benefit of being a self-contained and rigorous method. However, it is found to be not well-suited to 'long-term' analysis, due to the computational effort required. The risk analysis for the chosen examples is presented, as well as an investigation of the robustness of the method when applied to complex and 'long-period' simulations.
机译:随着提议和已实施的具有各种飞行目标的星座系统的泛滥,评估空间碎片对低地球轨道卫星星座造成的危害越来越重要。这尤其适用于当前的基于星座的商业通信系统,因为它们通常部署在空间碎片环境中存在峰值的高度。使用两个星座配置示例,在分解事件之后的长达1个月的时间内执行影响风险分析。第一个类似于IRIDIUM系统,在大约800 km的高度包含近70颗近极轨道卫星,第二个类似于Globalstar的配置,在1400 km的高度具有56颗卫星,分布在倾斜52°的轨道平面上。使用SDS软件执行分析,该软件应用概率连续谱动力学技术。这具有作为一种独立且严格的方法的好处。但是,由于所需的计算量,发现它不适合“长期”分析。介绍了所选示例的风险分析,以及对应用于复杂和“长期”仿真的方法的鲁棒性进行了研究。

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