{"title":"用于太空助推器的低成本GPS惯性制导(GPSIG)","authors":"S. C. Maki","doi":"10.1109/PLANS.1990.66174","DOIUrl":null,"url":null,"abstract":"The GPS (Global Positioning System) application requirements for a variety of space vehicles, including the Space Transport Vehicle (STV), the Orbital Maneuvering Vehicle (OMV), the heavy lift launch vehicles of the Advanced Launch Systems (ALS) family and the Shuttle C (cargo), space platforms, and future manned vehicles, are summarized. GPS usage on unmanned space boosters is examined in greater depth. The requirements in the areas of performance, operational constraints, redundancy/reliability, implementation, and life cycle cost are detailed. Variations from the typical GPS/INS (inertial navigation system) integration approach are presented, including deletion of some inertial sensors, various types of inertial sensors, and multiplexed and separate channel receivers.<<ETX>>","PeriodicalId":156436,"journal":{"name":"IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences","volume":"1 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1990-03-20","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"2","resultStr":"{\"title\":\"A low-cost GPS inertial guidance (GPSIG) for space boosters\",\"authors\":\"S. C. Maki\",\"doi\":\"10.1109/PLANS.1990.66174\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The GPS (Global Positioning System) application requirements for a variety of space vehicles, including the Space Transport Vehicle (STV), the Orbital Maneuvering Vehicle (OMV), the heavy lift launch vehicles of the Advanced Launch Systems (ALS) family and the Shuttle C (cargo), space platforms, and future manned vehicles, are summarized. GPS usage on unmanned space boosters is examined in greater depth. The requirements in the areas of performance, operational constraints, redundancy/reliability, implementation, and life cycle cost are detailed. Variations from the typical GPS/INS (inertial navigation system) integration approach are presented, including deletion of some inertial sensors, various types of inertial sensors, and multiplexed and separate channel receivers.<<ETX>>\",\"PeriodicalId\":156436,\"journal\":{\"name\":\"IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences\",\"volume\":\"1 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1990-03-20\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"2\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/PLANS.1990.66174\",\"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 Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/PLANS.1990.66174","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
A low-cost GPS inertial guidance (GPSIG) for space boosters
The GPS (Global Positioning System) application requirements for a variety of space vehicles, including the Space Transport Vehicle (STV), the Orbital Maneuvering Vehicle (OMV), the heavy lift launch vehicles of the Advanced Launch Systems (ALS) family and the Shuttle C (cargo), space platforms, and future manned vehicles, are summarized. GPS usage on unmanned space boosters is examined in greater depth. The requirements in the areas of performance, operational constraints, redundancy/reliability, implementation, and life cycle cost are detailed. Variations from the typical GPS/INS (inertial navigation system) integration approach are presented, including deletion of some inertial sensors, various types of inertial sensors, and multiplexed and separate channel receivers.<>
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