用于低推力往返任务的近地小行星调查

Ruida Xie, A. Dempster
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引用次数: 2

摘要

本研究的目的是对近地小行星(NEAs)进行广泛的低推力(LT)往返可达性分析。对近地天体的脉冲任务已经从不同的角度进行了研究,而近地天体的低推力任务由于低推力轨道设计的复杂性而没有得到适当的研究。构建并训练了一个深度神经网络分类器来预测地球和近地天体之间低推力转移的可行性。该模型预测准确率达98%,可用于过滤不可行转移,提高搜索效率。构建并训练深度神经网络(DNN)回归器作为LT优化过程的代理。dnn回归器输出的航天器最终质量预测平均相对误差(MRE)小于1%。这两个模型被集成到一个网格搜索框架中,可以对LT行程进行有效的搜索。对于给定的航天器配置,研究的24,149个近地天体中有7%(1,684个)是可LT往返的,95.4%可LT往返的最小推进剂质量分数在0.08到0.29之间。经鉴定的可接近的低低温nea的倾斜度小于9度,偏心率小于0.4。一些小行星,如2017cf32,被发现使用低推力推进选项比脉冲推进选项更容易接近。研究结果可为今后低推力NEA任务目标的选择提供参考。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A Survey of Near-Earth Asteroids for Low-Thrust Round-Trip Missions
The objective of this study is to perform a broad low thrust (LT) round-trip accessibility analysis for near-Earth asteroids (NEAs). The impulsive missions to NEAs have been investigated in several studies from various perspectives, while NEAs' low-thrust missions have not been properly investigated due to the complexity of LT trajectory design. A Deep Neural Network (DNN) classifier is constructed and trained to predict the feasibility of low thrust transfers between Earth and NEAs. This model has a prediction accuracy of 98%, and it is used for filtering out infeasible transfers and enhance the search efficiency. A Deep Neural Network (DNN) regressor is constructed and trained as the surrogate of the LT optimization process. The DNN-regressor outputs the spacecraft final mass with a prediction mean-relative error (MRE) of less than 1%. These two models are integrated into a grid search framework and enable efficient searches for LT journeys. For the given spacecraft configurations, 7% (1,684) of the 24,149 studied NEAs are LT round-trip accessible, and 95.4% of the LT accessible ones have minimum propellant mass fractions between 0.08 and 0.29. The identified LT accessible NEAs have inclinations less than 9 deg and eccentricities less than 0.4. Some asteroids, such as 2017 CF32, are found to be more accessible by the low-thrust propulsion option than the impulsive propulsion. The results of this study can be used as a reference for future low-thrust NEA mission target selection.
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