发明名称 Verfahren und Vorrichtung zum Anzeigen von Steuerungsschwingungskupplungen in einem Flugzeug
摘要 A pilot control (1) and transductor (4) produce a signal (delta) which moves a control surface (8) through a calculator (6) and actuator (7). The transductor signals are filtered (10) to exclude those outside 0.3-0.6 Hz, then selectively sampled and subjected to Fourier analysis (11). The two leading Fourier coefficients are used with the number of samples to find an index which is compared to a fraction of the maximum transductor signal An Independent claim is also included for : Equipment able to sample the signals, make a Fourier analysis, calculate an index, compare the index to a fraction of the maximum signal and determine if pilot induced oscillations are present
申请公布号 DE60304142(T2) 申请公布日期 2006.09.28
申请号 DE2003604142T 申请日期 2003.10.23
申请人 AIRBUS FRANCE 发明人 RAIMBAULT, NATHALIE;FABRE, PIERRE
分类号 G05D1/08 主分类号 G05D1/08
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