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    FLIGHT CONTROL DEVICE
    1.
    发明公开
    FLIGHT CONTROL DEVICE 审中-实审

    公开(公告)号：EP4428041A1

    公开(公告)日：2024-09-11

    申请号：EP22889785.6

    申请日：2022-10-20

    申请人： DENSO CORPORATION

    发明人： TAKEMURA, Yuichi

    IPC分类号： B64D45/00 ,  B64C13/18 ,  B64C27/24 ,  B64C39/02 ,  B64D27/24 ,  B64D47/08 ,  G01C21/20 ,  G08G5/00 ,  G08G5/04

    CPC分类号： B64C13/18 ,  B64C27/24 ,  B64C39/02 ,  B64D27/24 ,  B64D45/00 ,  B64D47/08 ,  G01C21/20 ,  G08G5/00 ,  G08G5/04

    摘要： A flight control device performs flight control processing for causing a subject aircraft to fly. When a collision between the subject aircraft and a counterpart aircraft is predicted, the flight control device performs detection avoidance processing assuming that a risk of collision has been detected. In step S304 of the detection avoidance processing, the flight control device sets an order of priority of the subject aircraft and the counterpart aircraft for collision avoidance. When the order of priority of the counterpart aircraft is higher than the order of priority of the subject aircraft, it is assumed that the counterpart aircraft performs collision avoidance flight, and the flight control device (40) ends the detection avoidance processing without performing the collision avoidance flight. On the other hand, when the order of priority of the subject aircraft is higher than the order of priority of the counterpart aircraft, the flight control device changes a flight route of the subject aircraft to the collision avoidance route in step S404.

    ENHANCED GROUND PROXIMITY WARNING SYSTEM THAT SELECTIVELY OPERATES IN BOTH A HELICOPTER MODE AND A FIXED-WING MODE
    5.
    发明公开
    ENHANCED GROUND PROXIMITY WARNING SYSTEM THAT SELECTIVELY OPERATES IN BOTH A HELICOPTER MODE AND A FIXED-WING MODE 审中-公开

    公开(公告)号：EP4266288A1

    公开(公告)日：2023-10-25

    申请号：EP23165369.2

    申请日：2023-03-30

    申请人： Honeywell International Inc.

    发明人： ISHIHARA, Yasuo ,  GON, Supratik

    IPC分类号： G08G5/00 ,  G08G5/04

    摘要： A system and method are provided for controlling operations of an enhanced ground proximity warning system (EGPWS) disposed within an aircraft that is configured to selectively operate in both a helicopter mode and a fixed-wing mode. A processor processes one or more aircraft flight parameters to determine when the aircraft is operating in the helicopter mode and when the aircraft is operating in the fixed-wing mode. The EGPWS is commanded, via the processor, to operate as a helicopter EGPWS when the aircraft is operating in the helicopter mode, and is commanded, via the processor, to operate as a fixed-wing EGPWS when the aircraft is operating in the fixed-wing mode.

    VEHICLE NAVIGATION ASSISTANCE
    9.
    发明公开
    VEHICLE NAVIGATION ASSISTANCE 审中-公开

    公开(公告)号：EP4198945A1

    公开(公告)日：2023-06-21

    申请号：EP21275186.1

    申请日：2021-12-16

    申请人： BAE SYSTEMS plc

    发明人： The designation of the inventor has not yet been filed

    IPC分类号： G08G5/00 ,  G08G5/04

    摘要： A mobile communication device (102) of a vehicle (103) is associated with a navigation system (202). Vehicle navigational data derived from the navigation system (202) is received, via cellular network communication, from the mobile communication device (102) of a vehicle (103). The vehicle navigational data is used to determine that a navigation assistance notification should be communicated to the mobile communication device (102) and, in response, communication of the navigation assistance notification to the mobile communication device (102) is initiated.