According to this invention, an aerial vehicle can be provided that reduces the effect of wind in a given direction striking its frame during flight of the aerial vehicle, thereby improving fuel consumption and stability. The aerial vehicle of this invention is equipped with a flight part including a frame to which a plurality of rotor blades including at least a propeller and a motor are connected, wherein the frame includes a right frame and a left frame extending side by side in the front-rear direction of the aerial vehicle, and at least one of the right frame and the left frame has a substantially wing-shaped portion with a leading edge located outside the aerial vehicle and a trailing edge located inside the aerial vehicle relative to a vertical center line in the frame. The substantially wing-shaped shape is a symmetrical wing shape.

Systems, apparatus, and methods are presented for testing a device. One method includes activating an actuator device to cause a carriage, coupled to a device, to be moved in one or more directions along a guide rail, wherein the device includes at least one processing device and one or more sensor devices. The method may also comprise receiving, by the device, one or more input commands and executing, by the device based on the one or more input commands, a software application to generate an output while the device is moving in the one or more directions. Further, the method may comprise verifying the execution of the software application on the device based on the output.

Systems, apparatus, and methods are presented for testing a device. One method includes activating an actuator device to cause a carriage, coupled to a device, to be moved in one or more directions along a guide rail, wherein the device includes at least one processing device and one or more sensor devices. The method may also comprise receiving, by the device, one or more input commands and executing, by the device based on the one or more input commands, a software application to generate an output while the device is moving in the one or more directions. Further, the method may comprise verifying the execution of the software application on the device based on the output.

Eyewear configured to control an unmanned aerial vehicle (UAV). In one example, a user interacts with the eyewear to generate control signals that are transmitted to the UAV to control the flight path, speed, orientation, and to communicate other instructions to the UAV. An input of the eyewear is controlled by the user to control the UAV, such as a touchpad, a microphone, a head movement tracker and a camera. The user is also able to configure and customize the eyewear to send specific control signals to the UAV as a function of user actions. This includes specific head movements and head gestures of the user as a method of controlling the UAV. This allows the user to control the UAV in a more natural and convenient way.

Eyewear configured to control an unmanned aerial vehicle (UAV). In one example, a user interacts with the eyewear to generate control signals that are transmitted to the UAV to control the flight path, speed, orientation, and to communicate other instructions to the UAV. An input of the eyewear is controlled by the user to control the UAV, such as a touchpad, a microphone, a head movement tracker and a camera. The user is also able to configure and customize the eyewear to send specific control signals to the UAV as a function of user actions. This includes specific head movements and head gestures of the user as a method of controlling the UAV. This allows the user to control the UAV in a more natural and convenient way.

A flying apparatus includes a main body assembly, an arm extending from the main body assembly, and a rotor attached to the arm. The arm includes a plurality of rods extending in juxtaposition with each other. The rotor is supported by the plurality of rods.

A flying apparatus includes a main body assembly, an arm extending from the main body assembly, and a rotor attached to the arm. The arm includes a plurality of rods extending in juxtaposition with each other. The rotor is supported by the plurality of rods.

A flying apparatus includes a main body assembly, a plurality of arms extending from the main body assembly, a plurality of rotors each attached to one of the plurality of arms, and an engine to supply a driving force to the rotors. The plurality of rotors include a first-side rotor and a second-side rotor such that, in a plan view, the first-side rotor is positioned on a first side of the engine and the second-side rotor is positioned on a second side of the engine opposite the first side. The engine includes a first output shaft to supply a driving force to the first-side rotor and a second output shaft to supply a driving force to the second-side rotor.

A flying apparatus includes a main body assembly, a plurality of arms extending from the main body assembly, a plurality of rotors each attached to one of the plurality of arms, and an engine to supply a driving force to the rotors. The plurality of rotors include a first-side rotor and a second-side rotor such that, in a plan view, the first-side rotor is positioned on a first side of the engine and the second-side rotor is positioned on a second side of the engine opposite the first side. The engine includes a first output shaft to supply a driving force to the first-side rotor and a second output shaft to supply a driving force to the second-side rotor.

A flying apparatus includes an airframe and a plurality of rotors attached to the airframe. The plurality of rotors include a main rotor and a sub-rotor. The airframe includes a main body assembly and an arm which extends from the main body assembly and to which the sub-rotor is attached at a distal end portion thereof. The main body assembly includes a framed main body on which a driver to drive the main rotor is mounted, and a projecting frame which projects from the framed main body and to which the main rotor is attached. A proximal end of the arm is connected to the projecting frames of the main body assembly.