{"title":"A new method for discriminating the Moon interference based on CES software","authors":"Zhijun Tu, Zhiwu Mei, Jun Yuan, Loulou Deng","doi":"10.1117/12.2028970","DOIUrl":null,"url":null,"abstract":"When the moon and the sun light enter into the field of view of the conical scanning earth sensor (CES), the real attitude of the spacecraft will be affected because of wrong CES measurements.To solve this problem, a new method based on the CES software can discriminate the interference effect.A series of ground are designed to verify this method effectiveness, and results indicate that this method can not only give a indication of the moon, but also can eliminate effect of the moon and the sun light on the CES’s measurements.Finally, the on-orbit flight data is presented to confirm this method validity.","PeriodicalId":344928,"journal":{"name":"Optics/Photonics in Security and Defence","volume":"483 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2013-10-30","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Optics/Photonics in Security and Defence","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1117/12.2028970","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0
Abstract
When the moon and the sun light enter into the field of view of the conical scanning earth sensor (CES), the real attitude of the spacecraft will be affected because of wrong CES measurements.To solve this problem, a new method based on the CES software can discriminate the interference effect.A series of ground are designed to verify this method effectiveness, and results indicate that this method can not only give a indication of the moon, but also can eliminate effect of the moon and the sun light on the CES’s measurements.Finally, the on-orbit flight data is presented to confirm this method validity.