{"title":"动态运动测量与自动分析技术及其在若干再入试验中的应用","authors":"A. Waterfall","doi":"10.1109/TA.1965.4319805","DOIUrl":null,"url":null,"abstract":"An automatic technique, utilizing a large high speed computer for the analysis of records obtained from accelerometers, pressure guages and gyros installed in the re-entry vehicles of the Black Knight rocket, is described. It is shown that this enables a suitable arrangement of only three accelerometers to yield trajectory data, angular motion and the aerodynamic characteristics of the re-entry body. Examples of the analysis of accelerometer and rate gyro data are given and the lines of further development and some applications are indicated.","PeriodicalId":13050,"journal":{"name":"IEEE Transactions on Aerospace","volume":null,"pages":null},"PeriodicalIF":0.0000,"publicationDate":"1965-06-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"2","resultStr":"{\"title\":\"Techniques of Measurement and Automatic Analysis of Dynamic Motion with Application to Some Re-Entry Experiments\",\"authors\":\"A. Waterfall\",\"doi\":\"10.1109/TA.1965.4319805\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"An automatic technique, utilizing a large high speed computer for the analysis of records obtained from accelerometers, pressure guages and gyros installed in the re-entry vehicles of the Black Knight rocket, is described. It is shown that this enables a suitable arrangement of only three accelerometers to yield trajectory data, angular motion and the aerodynamic characteristics of the re-entry body. Examples of the analysis of accelerometer and rate gyro data are given and the lines of further development and some applications are indicated.\",\"PeriodicalId\":13050,\"journal\":{\"name\":\"IEEE Transactions on Aerospace\",\"volume\":null,\"pages\":null},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1965-06-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"2\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"IEEE Transactions on Aerospace\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/TA.1965.4319805\",\"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 Aerospace","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/TA.1965.4319805","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Techniques of Measurement and Automatic Analysis of Dynamic Motion with Application to Some Re-Entry Experiments
An automatic technique, utilizing a large high speed computer for the analysis of records obtained from accelerometers, pressure guages and gyros installed in the re-entry vehicles of the Black Knight rocket, is described. It is shown that this enables a suitable arrangement of only three accelerometers to yield trajectory data, angular motion and the aerodynamic characteristics of the re-entry body. Examples of the analysis of accelerometer and rate gyro data are given and the lines of further development and some applications are indicated.
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