King Abdullah University of Science and Technology

Saudi Arabian Oil Company

Mohammad Z Shaqura

Jeff S Shamma

Fadl Abdellatif

Christian Claudel

Khalid Fahad Alzuhair

Samet Guler

Mohammed Algarni

A vehicle is guided from an initial position to a target position using a projection of a laser beam on a target. A set of waypoints from the initial position of the vehicle to a position proximate to the target position is determined using an orientation of a laser pointer that projects the laser beam and based on projection of the UAV initial position onto the laser beam pointing at the target. The vehicle is guided along the set of determined waypoints to the position proximate to the target position. The vehicle is guided from the position proximate to the target position using the optical system of the vehicle responsive to detection of a dot of the laser beam on the target by an optical system of the vehicle.

Controlling a vehicle using a remotely located laser and an on-board camera

A gripper mechanism for gripping a load, the gripper mechanism including a body, a first actuator mechanism attached to the body and configured to linearly move a first gripping device; and a second actuator mechanism attached to the body and configured to rotate a second gripping device. A translation of the first gripping device and a rotation of the second gripping device result in gripping the load.

Gripper mechanism and method

Systems and methods to protect the flight envelope in both manual flight and flight by a commercial autopilot are provided. A system can comprise: an inertial measurement unit (IMU); a computing device in data communication with the IMU; an application executable by the computing device comprising: logic that estimates an angle of attack; a slip angle; and a speed of an unmanned aerial vehicle (UAV) based at least in part on data received from the UAV. A method can comprise estimating, via a computing device, flight data of a UAV based at least in part on data received from an IMU; comparing the estimated flight data with measured flight data; and triggering an error indication in response to a determination that the measured flight data exceeds a predefined deviation of the estimated flight data. The estimated speed can comprise an estimated airspeed, vertical speed and/or ground velocity.

Flight envelope protection system for unmanned aerial vehicles

Growing community of inventors

Thuwal, Saudi Arabia

Mohammad Z Shaqura