发明名称 DEVICE AND METHOD FOR ASSISTING WITH RECONFIGURATION OF AN AIRCRAFT, AIRCRAFT INCLUDING SUCH A DEVICE AND ASSOCIATED COMPUTER PROGRAM PRODUCT
摘要 A device and method for assisting with reconfiguration of an aircraft, an aircraft including such a device and an associated computer program product are disclosed. In one aspect, the aircraft has an operational configuration, is configured to move in an operational environment, and includes at least one avionic system, at least one avionic member, and at least one monitoring system configured to detect an abnormality of an avionic member or a perturbation of the operational environment and to generate a fault information. The device is connected between at least one monitoring system and at least one avionic system, and includes a reception module configured to receive a fault information from the monitoring system, an impact computation module configured to compute an impact on the operational configuration of the aircraft, and a transmission module configured to transmit the computed impact to at least one avionic system.
申请公布号 US2015187148(A1) 申请公布日期 2015.07.02
申请号 US201414565871 申请日期 2014.12.10
申请人 THALES 发明人 SANNINO Christian;CHAZOTTES Xavier;COULMEAU Francois
分类号 G07C5/08;B64D45/00 主分类号 G07C5/08
代理机构 代理人
主权项 1. A device for assisting with reconfiguration of an aircraft, the aircraft having an operational configuration at a given instant, configured to move in an operational environment and including i) at least one avionic system, ii) at least one avionic member, the avionic member being connected to the avionic system for piloting the aircraft, and iii) at least one monitoring system configured to detect an abnormality of the avionic member or a perturbation of the operational environment and to generate fault information relating to the abnormality or to the perturbation, the device being connected between the monitoring system and the avionic system, the device comprising: a reception module configured to receive the fault information from the monitoring system;an impact computation module configured to compute, depending on the received fault information, at least one impact on the operational configuration of the aircraft; and a transmission module configured to transmit the computed impact to the avionic system.
地址 NEUILLY SUR SEINE FR