An unmanned aerial system includes a remote controller device and an unmanned aerial vehicle. A user input on the remote controller device indicates a flight command requested by a user. The remote controller device determines a current position and/or orientation of the remote controller device in response to the flight command from the user. The current position and/or orientation is sent to the vehicle. The vehicle responsively determines a desired orientation of the unmanned aerial vehicle as a function of the current position and/or orientation of the remote controller device and operates a lift mechanism to execute a flight operation based on the desired orientation of the unmanned aerial vehicle and the current position of the remote controller device.

Various embodiments include methods, devices, and robotic vehicle processing devices implementing such methods for automatically adjusting the minimum distance that a robotic vehicle is permitted to approach an object by a collision avoidance system based upon a classification or type of object.

A smart nozzle assembly includes a nozzle, a nozzle control mechanism, and camera rigidly attached to the nozzle for use with a mobile robot in an autonomous spray painting system. The nozzle control mechanism is configured to control flowrate, control the shape of the spray pattern, mix two or more colors, and clean dried paint at the nozzle tip. The nozzle assembly further includes a process for running software to manage or initiate the nozzle control mechanism's functionality and to provide the nozzle calibration. The calibration method for the nozzle uses a novel algorithm that measures the spray pattern, the distribution of paint within the spray pattern, and the relative position of the nozzle and camera. The distribution of paint within the spray pattern is measured in terms of physical quantity of delivered paint per unit area.

An aerial vehicle having a single wing is configured for vertical-flight and forward-flight operations. The wing has a substantially high aspect ratio. The aerial vehicle includes tilt motor assemblies disposed at a forward end and an aft end of a fuselage. The tilt motor assemblies are configured to orient motors and rotors vertically, horizontally, or at any angle between vertical and horizontal. A pair of parallel booms are mounted beneath the wing on either side of the fuselage. Each of the booms has at least one vertically oriented motor and rotor associated therewith, and a vertical fin extending thereunder. Additionally, a forward tilt motor assembly includes a rotatable extension that is deployed when the motor assembly is configured for vertical flight, enabling the aerial vehicle to land on the vertical fins and the landing rotatable extension.

Unmanned aerial vehicle (UAV) including a flight propulsion system and a support system coupled to the flight propulsion system, the support system comprising a protective outer cage configured to surround the flight propulsion system, wherein the outer cage comprises a plurality of cage frame modules that are manufactured as separate components and assembled together to form at least a portion of the outer cage configured to surround the flight propulsion system.

Described herein are apparatuses that provided various features related to unmanned aerial vehicles (UAVs). An example apparatus may include, among other features, (i) a launch system for a UAV, (ii) a landing feature that is arranged on the apparatus so as to receive the UAV when the UAV returns from a flight, and (iii) a mechanical battery-replacement system that is configured to (a) remove a first battery from the UAV, and (b) after removal of the first battery, install a second battery in the UAV.

A propeller guard 10 includes a frame 16 provided along a rotating surface of a propeller 30 and surrounding a rotating end 30b of the propeller 30, in which the frame 16 includes a plurality of protrusions 16b protruding outward in plan view.

A propeller guard 10 includes a frame 16 provided along a rotating surface of a propeller 30 and surrounding a rotating end 30b of the propeller 30, in which the frame 16 includes a plurality of protrusions 16b protruding outward in plan view.

A flying machine includes a flying machine body including a rotor blade; a frame including a frame body supporting the flying machine body, and a pressing section that is pressed against a target object at least at two locations separated along a direction orthogonal to a width direction of the frame body; and a detector fixed to the frame, and having a detection direction that is a direction orthogonal to a direction joining the two locations together and facing toward the target object.

Described is an apparatus and method of an aerial vehicle, such as an unmanned aerial vehicle (UAV) that can operate in either a vertical takeoff and landing (VTOL) orientation or a horizontal flight orientation. The aerial vehicle includes a plurality of propulsion mechanisms that enable the aerial vehicle to move in any of the six degrees of freedom (surge, sway, heave, pitch, yaw, and roll) when in the VTOL orientation. The aerial vehicle also includes a ring wing that surrounds the propulsion mechanisms and provides lift to the aerial vehicle when the aerial vehicle is operating in the horizontal flight orientation.