{"title":"用于低推力往返任务的近地小行星调查","authors":"Ruida Xie, A. Dempster","doi":"10.1109/AERO53065.2022.9843463","DOIUrl":null,"url":null,"abstract":"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.","PeriodicalId":219988,"journal":{"name":"2022 IEEE Aerospace Conference (AERO)","volume":"137 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2022-03-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"2","resultStr":"{\"title\":\"A Survey of Near-Earth Asteroids for Low-Thrust Round-Trip Missions\",\"authors\":\"Ruida Xie, A. Dempster\",\"doi\":\"10.1109/AERO53065.2022.9843463\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"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.\",\"PeriodicalId\":219988,\"journal\":{\"name\":\"2022 IEEE Aerospace Conference (AERO)\",\"volume\":\"137 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2022-03-05\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"2\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2022 IEEE Aerospace Conference (AERO)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/AERO53065.2022.9843463\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2022 IEEE Aerospace Conference (AERO)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/AERO53065.2022.9843463","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
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.