公开(公告)号：EP3020633A1

公开(公告)日：2016-05-18

申请号：EP15466013.8

申请日：2015-11-11

Applicant: Vyzkumny utav melioraci a ochrany pudy, v.v.l. ,  ADCIS s.r.o.

Inventor： Kulhavý, Zbynek ,  Krejzek, Pavel ,  Kulhavý, Martin

IPC: B64C39/02 ,  G05D1/08

CPC classification number: G05D1/0866 ,  B64C39/022 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/148

Abstract: The solution proposed refers to a flight control unit (6) for tied models (1) (copters; UAV - Unmanned Aerial Vehicle) that provides for direct flight control using mechanical or electronic guiding link (2) between the guiding point (3) and the model (1). The mechanical execution of the guiding point (3) and the guiding link (2) can consist of a whipcord, wire, electrical cable etc.; the electronic type of guiding link (2) is then representing the line with an acoustic or electromagnetic signal, a light beam etc. The unit may be completed with data communication to specify the position coordinates of the guiding point (3) and the model (1) in more detail. The solution proposed provides for fully automated navigation of the model (1) to a required position in reference of the guiding point (3), without imposing higher level of skills on the pilot (4) or the necessity to know the movement path trajectory in advance as it is the case in wireless remote control of the model (1), or its flight programming.

Abstract translation: 所提出的解决方案是指用于绑定型号（1）（直升机;无人机 - 无人机）的飞行控制单元（6），其使用机械或电子引导连杆（2）在引导点（3）和 模型（1）。 引导点（3）和引导连杆（2）的机械执行可以由拨号，电线，电缆等组成; 引导连杆（2）的电子式表示具有声或电信号，光束等的线。该单元可以用数据通信完成，以指定引导点（3）和模型（3）的位置坐标 1）更详细。 所提出的解决方案提供了将模型（1）的全自动导航参考引导点（3）到所需位置，而不对飞行员施加更高水平的技能（4）或者知道运动轨迹轨迹的必要性 如同在模型（1）的无线遥控器或其飞行编程中一样。