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Entry, Descent, And Landing Operations Analysis For The Stardust Entry Capsule

机译:星尘进入舱的进入,下降和着陆操作分析

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On the morning of 15 January 2006, the Stardust capsule successfully landed at the Utah Test and Training Range in northwest Utah, returning cometary samples from the comet Wild-2. An overview of the entry, descent, and landing trajectory analysis that was performed for targeting during the mission operations phase upon final approach to Earth is described. The final orbit determination solution produced an inertial entry flight-path angle of -8.21 deg (the desired nominal value) with a 3-σ uncertainty of ±0.0017 deg (2% of the requirement). The navigation and entry, descent, and landing operations effort accurately delivered the entry capsule to the desired landing site. The final landing location was 8.1 km from the target, which was well within the allowable landing area. Overall, the Earth approach operation procedures worked well and there were no issues (logistically or performance-based) that arose. As a result, the process of targeting a capsule from an interplanetary trajectory and accurately landing it on Earth was successfully demonstrated.
机译:2006年1月15日上午,星尘胶囊成功降落在犹他州西北部的犹他州测试和训练场,返回了来自Wild-2彗星的彗星样本。描述了进入,下降和着陆轨迹分析的概述,该分析是在任务操作阶段最终到达地球后针对目标进行的。最终的轨道确定解决方案产生了-8.21度(期望的标称值)的惯性进入飞行路径角,并且具有±0.0017度(要求的2%)的3-σ不确定度。导航和进入,下降和着陆操作的努力将进入舱准确地传送到所需的着陆点。最终的着陆位置距离目标8.1公里,这完全在允许的着陆区域内。总体而言,对地进近操作程序运行良好,没有出现任何问题(从逻辑上或基于性能的问题)。结果,成功地证明了从行星际轨道瞄准胶囊并将其准确降落到地球上的过程。

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