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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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