公开(公告)号：US20180057163A1

公开(公告)日：2018-03-01

申请号：US15245546

申请日：2016-08-24

Applicant: PRINCESS SUMAYA UNIVERSITY FOR TECHNOLOGY

Inventor： Belal Hussein Sababha ,  Hamzeh Mahmoud Alzu'bi ,  Osamah Ahmad Rawashdeh

IPC: B64C39/02 ,  B64C27/08 ,  B64C17/06

CPC classification number: B64C39/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/14

Abstract: A vertical take-off and landing (“VTOL”) unmanned aerial vehicle (“UAV”) system and a method of controlling the same, wherein such method controls the stability and maneuverability of the VTOL UAV by manipulating the speeds of the propellers at each rotor. The VTOL UAV includes a body with three extending arms, wherein each of such arms is aligned and fixed at a certain angle from a central axis passing through the body. Each extending arm is equipped with a rotor with propellers. The rotors are sufficient to control the yaw of the UAV, and there is no need for coaxial rotors or an extra servo-motor in order to control the yaw of the UAV, thus reducing the cost and the weight of the UAV.

公开(公告)号：US11560227B2

公开(公告)日：2023-01-24

申请号：US16280410

申请日：2019-02-20

Applicant: PRINCESS SUMAYA UNIVERSITY FOR TECHNOLOGY

Inventor： Belal Hussein Sababha ,  Hamzeh Mahmoud Alzu'bi ,  Osamah Ahmad Rawashdeh

IPC: B64C39/02 ,  G05D1/08

Abstract: A vertical take-off and landing (“VTOL”) unmanned aerial vehicle (“UAV”) system and a method of controlling the same, wherein such method controls the stability and maneuverability of the VTOL UAV by manipulating the speeds of the propellers at each rotor. The VTOL UAV includes a body with three extending arms, wherein each of such arms is aligned and fixed at a certain angle from a central axis passing through the body. Each extending arm is equipped with a rotor with propellers. The rotors are sufficient to control the yaw of the UAV, and there is no need for coaxial rotors or an extra servo-motor in order to control the yaw of the UAV, thus reducing the cost and the weight of the UAV.

公开(公告)号：US20190185160A1

公开(公告)日：2019-06-20

申请号：US16280410

申请日：2019-02-20

Applicant: PRINCESS SUMAYA UNIVERSITY FOR TECHNOLOGY

Inventor： Belal Hussein Sababha ,  Hamzeh Mahmoud Alzu'bi ,  Osamah Ahmad Rawashdeh

IPC: B64C39/02

CPC classification number: B64C39/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/14

Abstract: A vertical take-off and landing (“VTOL”) unmanned aerial vehicle (“UAV”) system and a method of controlling the same, wherein such method controls the stability and maneuverability of the VTOL UAV by manipulating the speeds of the propellers at each rotor. The VTOL UAV includes a body with three extending arms, wherein each of such arms is aligned and fixed at a certain angle from a central axis passing through the body. Each extending arm is equipped with a rotor with propellers. The rotors are sufficient to control the yaw of the UAV, and there is no need for coaxial rotors or an extra servo-motor in order to control the yaw of the UAV, thus reducing the cost and the weight of the UAV.