发明名称 |
Method and device for controlling an aircraft manoeuvring components, with electrical standby modules |
摘要 |
A device for controlling aircraft maneuvering units includes at least one control unit and a central computing unit. The control unit may be actuated by a pilot for issuing maneuvering commands. The central computing unit is capable of establishing control signals for at least one maneuvering unit from the maneuvering commands. Each central computing unit is being provided with its own failure detection system. The device further includes at least one backup electronic module respectively associated with a maneuvering unit and capable of also establishing control signals for this maneuvering unit from maneuvering commands. The electronic module lacks any failure detection system of its own, but it is connected to a central failure detection system. |
申请公布号 |
AU7758601(A) |
申请公布日期 |
2002.01.30 |
申请号 |
AU20010077586 |
申请日期 |
2001.07.12 |
申请人 |
AIRBUS FRANCE |
发明人 |
JEAN-MARC ORTEGA;JEAN-PIERRE GARCIA |
分类号 |
G05D1/00 |
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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