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2. 发明公开

KR1020110128255A 호버링이 가능한 항공기, 항공기 조종 보조 방법, 및 인터페이스 有权
标题翻译：飞机能力，航空器移动辅助方法和接口
公开(公告)号：KR1020110128255A
公开(公告)日：2011-11-29
申请号：KR1020110048757
申请日：2011-05-23
申请人： 아구스타 웨스트랜드 에스. 피. 에이.
发明人： 브루네티,마시모 , 고비,시몬 , 이아누치,다리오 , 마조리,에밀리오
IPC分类号： B64D45/00 , B64D47/00 , G05D1/10 , B64C27/04
CPC分类号： G08G5/045 , G01S13/94 , G05D1/0858 , G05D1/102 , G08G5/0078 , G08G5/0086
摘要： PURPOSE: An aircraft with a hovering function, a method of assisting the operation of an aircraft, and an interface are provided to enable a control unit to generate an alarm signal when at least on of first points is placed within a safe area comprising a second point on an aircraft by obtaining the distance values between the first points on an obstacle in a planar sweep area and the second point on the aircraft. CONSTITUTION: An aircraft with a hovering function comprises a body, a rotor(3), a driving shaft, at least one sensor(10), and a control unit. The rotor is mounted on the top of the body. The driving shaft is protruded from the body and drives the rotor. The sensor comprises a planar sweep area(R). While the aircraft flies, the sensor obtains each distance value between first values(P) on an obstacle(O) in the planar sweep area and a second point(Q) on the aircraft(1). When at least on of the first points is placed in a safe area(Z) comprising the second point on the aircraft, the control unit generates an alarm signal.
摘要翻译：目的：提供具有悬停功能的飞行器，辅助飞行器的操作的方法和接口，以使控制单元能够在至少在第一点上放置在安全区域内时产生报警信号，所述安全区域包括第二通过获得平面扫掠区域中的障碍物上的第一点与飞行器上的第二点之间的距离值来指向飞机。构成：具有悬停功能的飞机包括主体，转子（3），驱动轴，至少一个传感器（10）和控制单元。转子安装在车身的顶部。驱动轴从主体突出并驱动转子。传感器包括平面扫掠区域（R）。当飞机飞行时，传感器获得平面扫掠区域上的障碍物（O）上的第一值（P）和飞机（1）上的第二点（Q）之间的每个距离值。当第一点中的至少一个被放置在包括飞行器上的第二点的安全区域（Z）中时，控制单元产生报警信号。

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