发明名称 Modular electronic flight control system has actuator control-electronics having selection logic to decide whether to use directly received pilot guidelines or reference values of flight control processor for controlling actuator module
摘要 <p>Modular electronic flight control system has a number of actuator modules (10,11) and a number of Actuator Control-Electronics (ACEs) (20,21). Each individual actuator module is assigned with a particular ACE. The ACE directly receives pilot guidelines and the actuator module is controlled accordingly. The ACEs have a selection logic, which decides, whether to use the directly received pilot guidelines or the reference values of the primary flight control processor (30,31) for controlling the actuator module.</p>
申请公布号 DE102006039671(A1) 申请公布日期 2008.03.20
申请号 DE20061039671 申请日期 2006.08.24
申请人 LIEBHERR-AEROSPACE LINDENBERG GMBH 发明人 RIED, GEORG;HOFER, HERMANN
分类号 G05D1/00;B64C19/00 主分类号 G05D1/00
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