Burgess R. Johnson, Curt Albrecht, T. Braman, K. Christ, Patrick Duffy, D. Endean, M. Gnerlich, J. Reinke
{"title":"导航级MEMS IMU的研制","authors":"Burgess R. Johnson, Curt Albrecht, T. Braman, K. Christ, Patrick Duffy, D. Endean, M. Gnerlich, J. Reinke","doi":"10.1109/INERTIAL51137.2021.9430466","DOIUrl":null,"url":null,"abstract":"Performance data is presented from a MEMS-based IMU being developed at Honeywell with the objective of navigation-grade performance for a variety of applications. Design of the gyroscope is derived from that of the gyroscope in Honeywell's HG1930 tactical-grade MEMS IMU, a widely used tactical-grade MEMS IMU product. Fabrication processes similar to that of the gyroscope are used to fabricate a new vibrating beam accelerometer which measures acceleration via differential frequency change. Turn-on to turn-on bias repeatability better than 0.1 deg/hr for the gyroscopes and better than 20 micro-g for the accelerometers has been consistently demonstrated. Typical gyro ARW of 0.0035 deg/rt(hr) has been achieved, and accel root Allan variance is less than 10 micro-g at integration time of 1 second. The IMU has the same mechanical footprint (though slightly taller) and same electrical interface as Honeywell's HG1930 IMU.","PeriodicalId":424028,"journal":{"name":"2021 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL)","volume":"92 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2021-03-22","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"18","resultStr":"{\"title\":\"Development of a Navigation-Grade MEMS IMU\",\"authors\":\"Burgess R. Johnson, Curt Albrecht, T. Braman, K. Christ, Patrick Duffy, D. Endean, M. Gnerlich, J. Reinke\",\"doi\":\"10.1109/INERTIAL51137.2021.9430466\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Performance data is presented from a MEMS-based IMU being developed at Honeywell with the objective of navigation-grade performance for a variety of applications. Design of the gyroscope is derived from that of the gyroscope in Honeywell's HG1930 tactical-grade MEMS IMU, a widely used tactical-grade MEMS IMU product. Fabrication processes similar to that of the gyroscope are used to fabricate a new vibrating beam accelerometer which measures acceleration via differential frequency change. Turn-on to turn-on bias repeatability better than 0.1 deg/hr for the gyroscopes and better than 20 micro-g for the accelerometers has been consistently demonstrated. Typical gyro ARW of 0.0035 deg/rt(hr) has been achieved, and accel root Allan variance is less than 10 micro-g at integration time of 1 second. The IMU has the same mechanical footprint (though slightly taller) and same electrical interface as Honeywell's HG1930 IMU.\",\"PeriodicalId\":424028,\"journal\":{\"name\":\"2021 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL)\",\"volume\":\"92 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2021-03-22\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"18\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2021 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/INERTIAL51137.2021.9430466\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2021 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/INERTIAL51137.2021.9430466","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Performance data is presented from a MEMS-based IMU being developed at Honeywell with the objective of navigation-grade performance for a variety of applications. Design of the gyroscope is derived from that of the gyroscope in Honeywell's HG1930 tactical-grade MEMS IMU, a widely used tactical-grade MEMS IMU product. Fabrication processes similar to that of the gyroscope are used to fabricate a new vibrating beam accelerometer which measures acceleration via differential frequency change. Turn-on to turn-on bias repeatability better than 0.1 deg/hr for the gyroscopes and better than 20 micro-g for the accelerometers has been consistently demonstrated. Typical gyro ARW of 0.0035 deg/rt(hr) has been achieved, and accel root Allan variance is less than 10 micro-g at integration time of 1 second. The IMU has the same mechanical footprint (though slightly taller) and same electrical interface as Honeywell's HG1930 IMU.
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