发明名称 Device and method for controlling the validity of at least one parameter calculated by an aircraft anemometer station
摘要 The method involves calculating a difference between each information issued from an external information source (Si) and information depending on a parameter e.g. total pressure, calculated by a central anemometer (2) of an aircraft. An absolute value of the difference is compared to a threshold value. The parameter is found to be invalid if the absolute value is greater than the threshold value, or the parameter is valid. Independent claims are also included for the following: (a) a system to monitor validity of a parameter that is calculated by a central anemometer of an aircraft (b) an aircraft.
申请公布号 EP1496414(A1) 申请公布日期 2005.01.12
申请号 EP20040291556 申请日期 2004.06.21
申请人 AIRBUS FRANCE 发明人 D'OUINCE, ARNAUD;ANDREOLETTI, REMI
分类号 G01D3/08;G05B9/03;G05D1/00 主分类号 G01D3/08
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