{"title":"用于超高速战略系统和天基拦截器的自主恒星角参考系统","authors":"S. Levine, F. Nadeau, R. Miller","doi":"10.1109/PLANS.1992.185819","DOIUrl":null,"url":null,"abstract":"Summary form only given. The authors discuss a solid-state stellar angular reference system (STARS) augmented by a low-cost inertial navigator for precision endo exoatmospheric hypervelocity strategic weapon systems and space-based interceptors. Inertial instrument performance, sensor integration, the stellar image, star tracker signal-to-noise ratio, star density, telescope field of view, and physical size constraints that affect overall system performance have been examined. Some of the unique features of this work are miniature holographic optical element telescope, all-silicon micromechanical inertial instruments, hypervelocity plasma effects, and trajectory-induced errors.<<ETX>>","PeriodicalId":422101,"journal":{"name":"IEEE PLANS 92 Position Location and Navigation Symposium Record","volume":"13 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1992-03-23","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Autonomous stellar angular reference systems (STARS) for hypervelocity strategic systems and space based interceptors\",\"authors\":\"S. Levine, F. Nadeau, R. Miller\",\"doi\":\"10.1109/PLANS.1992.185819\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Summary form only given. The authors discuss a solid-state stellar angular reference system (STARS) augmented by a low-cost inertial navigator for precision endo exoatmospheric hypervelocity strategic weapon systems and space-based interceptors. Inertial instrument performance, sensor integration, the stellar image, star tracker signal-to-noise ratio, star density, telescope field of view, and physical size constraints that affect overall system performance have been examined. Some of the unique features of this work are miniature holographic optical element telescope, all-silicon micromechanical inertial instruments, hypervelocity plasma effects, and trajectory-induced errors.<<ETX>>\",\"PeriodicalId\":422101,\"journal\":{\"name\":\"IEEE PLANS 92 Position Location and Navigation Symposium Record\",\"volume\":\"13 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1992-03-23\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"IEEE PLANS 92 Position Location and Navigation Symposium Record\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/PLANS.1992.185819\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"IEEE PLANS 92 Position Location and Navigation Symposium Record","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/PLANS.1992.185819","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Autonomous stellar angular reference systems (STARS) for hypervelocity strategic systems and space based interceptors
Summary form only given. The authors discuss a solid-state stellar angular reference system (STARS) augmented by a low-cost inertial navigator for precision endo exoatmospheric hypervelocity strategic weapon systems and space-based interceptors. Inertial instrument performance, sensor integration, the stellar image, star tracker signal-to-noise ratio, star density, telescope field of view, and physical size constraints that affect overall system performance have been examined. Some of the unique features of this work are miniature holographic optical element telescope, all-silicon micromechanical inertial instruments, hypervelocity plasma effects, and trajectory-induced errors.<>