{"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}
引用次数: 2
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.
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