{"title":"陀螺质量不平衡自动测量技术","authors":"F. L. Walker","doi":"10.1109/TME.1963.4323039","DOIUrl":null,"url":null,"abstract":"An inertial navigation system containing a versatile computer can be given the capability of automatically measuring its gyro mass unbalance. These measurements are accomplished in tests performed and monitored by the computer. Mass-unbalanced drifts induced by tilting the stable platform are detected by the system's acceleration sensors. From the outputs of these sensors, the computer determines the mass-unbalance components using regression-analysis techniques that minimize errors of extraneous origin.","PeriodicalId":199455,"journal":{"name":"IEEE Transactions on Military Electronics","volume":"21 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":"{\"title\":\"An Automatic Gyro Mass-Unbalance Measuring Technique\",\"authors\":\"F. L. Walker\",\"doi\":\"10.1109/TME.1963.4323039\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"An inertial navigation system containing a versatile computer can be given the capability of automatically measuring its gyro mass unbalance. These measurements are accomplished in tests performed and monitored by the computer. Mass-unbalanced drifts induced by tilting the stable platform are detected by the system's acceleration sensors. From the outputs of these sensors, the computer determines the mass-unbalance components using regression-analysis techniques that minimize errors of extraneous origin.\",\"PeriodicalId\":199455,\"journal\":{\"name\":\"IEEE Transactions on Military Electronics\",\"volume\":\"21 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1900-01-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"1\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"IEEE Transactions on Military Electronics\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/TME.1963.4323039\",\"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 Transactions on Military Electronics","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/TME.1963.4323039","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
An Automatic Gyro Mass-Unbalance Measuring Technique
An inertial navigation system containing a versatile computer can be given the capability of automatically measuring its gyro mass unbalance. These measurements are accomplished in tests performed and monitored by the computer. Mass-unbalanced drifts induced by tilting the stable platform are detected by the system's acceleration sensors. From the outputs of these sensors, the computer determines the mass-unbalance components using regression-analysis techniques that minimize errors of extraneous origin.