发明名称 SYSTEMS AND METHODS FOR IMPROVED ACCURACY
摘要 <p>Systems and methods for determining turbine engine system stability encompass measuring or otherwise determining values of performance parameters, storing a data set of such values in memory, generating a stability indicator, and displaying the stability indicator on an operator interface. The stability indicator is generated by a processor operating in data communication with the computer memory, utilizing customized software algorithms to remove high frequency components, apply an adaptive filter to adjust selected parameters according to a target value of a selected target parameter, and apply a stochastic filters to estimate true values of the selected parameters, based on the remaining variation.</p>
申请公布号 CA2870512(A1) 申请公布日期 2015.05.12
申请号 CA20142870512 申请日期 2014.11.12
申请人 AERO SYSTEMS ENGINEERING, INC. 发明人 LONG, DEAN FREDERICK;SIMON, KENNETH WILLIAM;RADINZEL, GRANT AUGUST
分类号 G01M15/14 主分类号 G01M15/14
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