Abstract: An unmanned aerial vehicle includes a propulsion system having at least one propulsion module comprised of at least one propeller and at least two motors/engines, one or more of the motors/engines providing mechanical energy to drive the propeller, wherein the difference between the angular velocities of the motors/engines provides energy input to a mechanical or magneto-mechanical linkage system to change the blade pitch angle of the propeller, in cyclic and/or collective manner.

Abstract: An unmanned aerial vehicle includes a tubular base structure, a motor having a stator, the stator being connected to the tubular base structure, an energy storage module configured to supply power to the motor, and at least one propeller driven by the motor, wherein the tubular base structure houses at least one cable for routing power or signals, or a fuel conduit or wire conduit.

Abstract: A system for the automated landing of an unmanned aerial vehicle includes an unmanned aerial vehicle having a control module, a first remote control device located at a remote location and controllable by a pilot, the first remote control device being configured to communicate with the unmanned aerial vehicle, and a second remote control system device located at a landing area and controllable by an observer, the second remote control device being configured to communicate with the unmanned aerial vehicle. The first remote control device and the second remote control device are configured for continuous communication with the unmanned aerial vehicle for landing of the unmanned aerial vehicle at a landmark at the landing area.

Abstract: An unmanned aerial vehicle includes a propulsion system having at least one propulsion module comprised of at least one propeller and at least two motors/engines, one or more of the motors/engines providing mechanical energy to drive the propeller, wherein the difference between the angular velocities of the motors/engines provides energy input to a mechanical or magneto-mechanical linkage system to change the blade pitch angle of the propeller, in cyclic and/or collective manner.

Abstract: A system for the automated landing of an unmanned aerial vehicle includes an unmanned aerial vehicle having a control module, a first remote control device located at a remote location and controllable by a pilot, the first remote control device being configured to communicate with the unmanned aerial vehicle, and a second remote control system device located at a landing area and controllable by an observer, the second remote control device being configured to communicate with the unmanned aerial vehicle. The first remote control device and the second remote control device are configured for continuous communication with the unmanned aerial vehicle for landing of the unmanned aerial vehicle at a landmark at the landing area.

Abstract: An unmanned aerial vehicle includes a tubular base structure, a motor having a stator, the stator being connected to the tubular base structure, an energy storage module configured to supply power to the motor, and at least one propeller driven by the motor, wherein the tubular base structure houses at least one cable for routing power or signals, or a fuel conduit or wire conduit.

Abstract: A controller for an unmanned aerial vehicle includes a frame having a pair of opposed arms configured to removably receive a smart device therebetween, at least one point stick module positioned on at least one of the arms, and a control unit configured to establish and maintain a connection with the smart device. The at least one point stick module is operable by a user to control movement of the unmanned aerial vehicle.