A system and method of controlling quadrotor air vehicles (QRAV) that may include an additional two degrees of freedom for each of the four propellers of the QRAV. Each of the four rotors may be allowed to rotate (tilt) around two local axes selected from the x-axis (roll), y-axis (pitch), and z-axis (yaw). Control of the quadrotor including the additional two degrees of freedom allows thrust of each rotor to be direct in any direction of a semi-sphere. As a result, total control inputs of the QRAV may be increased to twelve, enabling smooth control to achieve superior and precise maneuverability. Additionally, the system and method is fault tolerant and capable of handling failures of any of the rotors. Commands to the propellers may be fully decoupled and achieved independently thereby giving pilots better control to execute difficult maneuvers.
SYSTEM AND METHOD FOR CONTROL OF QUADROTOR AIR VEHICLES WITH TILTABLE ROTORS
2016-01-28
Patent
Elektronische Ressource
Englisch
Quadrotor with tiltable rotors for manned applications
IEEE | 2014
|BASE | 2022
|Amphibious unmanned aerial vehicle with tiltable rotors
Europäisches Patentamt | 2021
|Vertical Takeoff and Landing Aircraft with Tiltable Rotors
Europäisches Patentamt | 2021
|