发明名称 ACTIVE PITCH CONTROL METHOD AND DEVICE FOR AN AIRCRAFT
摘要 The device (1) comprises means (4) for calculating a pitch acceleration instruction depending on a pitch objective and means (5) for calculating, from this pitch acceleration instruction, a deflection instruction for the elevators (7) of the aircraft.
申请公布号 US2010042270(A1) 申请公布日期 2010.02.18
申请号 US20070937935 申请日期 2007.11.09
申请人 AIRBUS FRANCE 发明人 VILLAUME FABRICE
分类号 G05D1/08;G06N3/02 主分类号 G05D1/08
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