公开(公告)号：WO2015195175A3

公开(公告)日：2016-02-11

申请号：PCT/US2015022001

申请日：2015-03-23

Applicant: BORKO BRANDON

Inventor： BORKO BRANDON

IPC: B64F1/04 ,  E04H6/44

CPC classification number: B64F1/04 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/08 ,  B64C2201/182 ,  B64C2201/201 ,  B64F1/12

Abstract: A system for facilitating automated landing and takeoff of an autonomous or pilot controlled hovering air vehicle with a cooperative underbody at a stationary or mobile landing place and an automated storage system used in conjunction with the landing and takeoff mechanism that stores and services a plurality of UAVs is described. The system is primarily characterized in that the landing mechanism is settable with 6 axes in roll, pitch, yaw, and x, y and z and becomes aligned with and intercepts the air vehicle in flight and decelerates the vehicle with respect to vehicle's inertial limits. The air vehicle and capture mechanism are provided with a transmitter and receiver to coordinate vehicle priority and distance and angles between landing mechanism and air vehicle. The landing and takeoff system has means of tracking the position and orientation of the UAV in real time. The landing mechanism will be substantially aligned to the base of the air vehicle. With small UAVs, their lifting capacity is limited. Reducing sensing and computation requirements by having the landing plate perform the precision adjustments for the landing operation allows for increased flight time and/or payload capacity.

Abstract translation: 一种用于促进自主着陆和起飞的自动着陆和起飞的自动着陆控制悬停飞行器，其具有在固定或移动着陆地点的协作车身，以及与着陆和起飞机构结合使用的自动存储系统，其存储和服务多个UAV 被描述。 该系统的主要特征在于，着陆机构可设置为具有卷轴，俯仰，偏航以及x，y和z的6个轴线，并且与飞行中的空中车辆对准并拦截，并使车辆相对于车辆的惯性极限减速。 机动车辆和捕获机构设置有发射器和接收器，以协调车辆优先级，着陆机构和空中车辆之间的距离和角度。 着陆和起飞系统具有实时跟踪无人机的位置和方向的手段。 着陆机构将基本上与机动车辆的底座对准。 对于小型无人机，起重能力有限。 通过使着陆板执行着陆操作的精确调整来减少感测和计算要求，可以增加飞行时间和/或有效负载能力。