{"title":"ExoMars雷达多普勒高度计在下降舱姿态重建中的应用研究","authors":"M. Iorio, P. Pepe, Michela Veredice","doi":"10.1109/METROAEROSPACE.2018.8453569","DOIUrl":null,"url":null,"abstract":"This paper describes a simple methodology to evaluate the attitude of the ExoMars Entry Descent and landing Demonstrator Module (EDM), called Schiaparelli Module, using the Ka band Radar Doppler Altimeter (RDA) range and velocity measurements. This approach is attractive to improve the EDM navigation system robustness. The proposed methodology has been verified during the RDA test campaign performed in Morocco (Mars like scenario) and applied to the experimental data recorded during the descent of the Schiaparelli Module on Mars.","PeriodicalId":142603,"journal":{"name":"2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace)","volume":"45 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2018-06-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"On the use of ExoMars Radar Doppler Altimeter for Descent Module Attitude Reconstruction\",\"authors\":\"M. Iorio, P. Pepe, Michela Veredice\",\"doi\":\"10.1109/METROAEROSPACE.2018.8453569\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"This paper describes a simple methodology to evaluate the attitude of the ExoMars Entry Descent and landing Demonstrator Module (EDM), called Schiaparelli Module, using the Ka band Radar Doppler Altimeter (RDA) range and velocity measurements. This approach is attractive to improve the EDM navigation system robustness. The proposed methodology has been verified during the RDA test campaign performed in Morocco (Mars like scenario) and applied to the experimental data recorded during the descent of the Schiaparelli Module on Mars.\",\"PeriodicalId\":142603,\"journal\":{\"name\":\"2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace)\",\"volume\":\"45 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2018-06-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/METROAEROSPACE.2018.8453569\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/METROAEROSPACE.2018.8453569","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
On the use of ExoMars Radar Doppler Altimeter for Descent Module Attitude Reconstruction
This paper describes a simple methodology to evaluate the attitude of the ExoMars Entry Descent and landing Demonstrator Module (EDM), called Schiaparelli Module, using the Ka band Radar Doppler Altimeter (RDA) range and velocity measurements. This approach is attractive to improve the EDM navigation system robustness. The proposed methodology has been verified during the RDA test campaign performed in Morocco (Mars like scenario) and applied to the experimental data recorded during the descent of the Schiaparelli Module on Mars.