Abstract:
Method and apparatus of prompting a position of an aerial vehicle are provided. The method may include: obtaining first position information of the aerial vehicle and second position information of a ground end; and presenting a relative position relationship between the aerial vehicle and the ground end on a preset map according to the first position information and the second position information. Flight status including flight position and other suitable information of an aerial vehicle may therefore be directly provided.
Abstract:
Techniques for determining whether data associated with an autonomous navigation of an unmanned vehicle may be trusted. For example, navigation-related data may be provided from a source external to the unmanned vehicle. Image data associated with the autonomous navigation may be generated. The navigation-related data and the image data may be compared to determine whether the navigation data may be trusted or not. If untrusted, the autonomous navigation may be directed independently of the navigation data.
Abstract:
A method for supporting target tracking includes acquiring a target from one or more images captured by an imaging device carried by a movable object, obtaining a relative distance between the movable object and the target, and generating one or more control signals based on the relative distance to direct the movable object to track the target.
Abstract:
A method of emergency handling is provided for a vehicle engaged with an uninhabited aerial vehicle (UAV). The method can include collecting location information if emergency situation occurs. In emergency situations, the vehicle can determine whether an operation of uninhabited aerial vehicle (UAV) is allowed based on the location information and time information. After determining whether there is a flight space for the operation of uninhabited aerial vehicle (UAV) above a vehicle, the vehicle can transmit at least one of SOS and an emergency call into the uninhabited aerial vehicle (UAV).
Abstract:
Innovative new systems and method of operating the systems, wherein the system comprises an airborne platform comprising an unmanned balloon; a payload that is separate from the unmanned balloon; a transceiver; first and second flight termination devices; at least two separate power sources for the first and second flight termination devices; a sensor; a processor; a pump; a valve; and a tether that when broken separates the unmanned balloon and the payload, are disclosed herein.
Abstract:
An unmanned aerial vehicle (UAV) detecting method is executed and applied in an UAV. The method can include creating a sample features database for a user, and storing the sample features database in a storage device; shooting a plurality of scene images from every direction around the user; capturing a plurality of features of the object from the scene image; comparing the sample features of user with the features of the object, and storing a new feature of the object different from the sample feature of user in the storage device; determining whether a tagger is around the user, and sending an alarm signal to the user.
Abstract:
An amphibious vertical takeoff and landing (VTOL) unmanned device includes a modular and expandable waterproof body. An outer body shell, at least one wing, and a door are connected to the modular and expandable waterproof body. A propulsion system of the amphibious VTOL unmanned device includes a plurality of motors and propellers and a propeller protection system. The amphibious VTOL unmanned device further includes a battery, a charging station for batteries, an onboard electricity generator a power distribution board, an electrical power storage device, and an electrical machine electrically connected to the electrical power storage device. The amphibious VTOL unmanned device is further equipped with a landing system, an onboard air compressor, an onboard electrolysis system, a cooling device, vision aiding and orientative lights, an apparatus for internally housing a cargo, and a manually or automatically deployable parachute.
Abstract:
An Unmanned Aerial Vehicle (UAV)-based installation method for equipment on cell towers includes flying the UAV with the equipment attached thereto upwards to a desired location on the cell tower, wherein the desired location comprises one or more horizontal support structures; positioning the equipment to the desired location on the cell tower; connecting the equipment to the desired location; and disconnecting the equipment from the UAV.
Abstract:
Disclosed is a configuration to control automatic return of an aerial vehicle. The configuration stores a return location in a storage device of the aerial vehicle. The return location may correspond to a location where the aerial vehicle is to return. One or more sensors of the aerial vehicle are monitored during flight for detection of a predefined condition. When a predetermined condition is met a return path program may be loaded for execution to provide a return flight path for the aerial vehicle to automatically navigate to the return location.
Abstract:
A vehicle-based airborne wind turbine system having an aerial wing, a plurality of rotors each having a plurality of rotatable blades positioned on the aerial wing, an electrically conductive tether secured to the aerial wing and secured to a ground station positioned on a vehicle, wherein the aerial wing is adapted to receive electrical power from the vehicle that is delivered to the aerial wing through the electrically conductive tether; wherein the aerial wing is adapted to operate in a flying mode to harness wind energy to provide a first pulling force through the tether to pull the vehicle; and wherein the aerial wing is also adapted to operate in a powered flying mode wherein the rotors may be powered so that the turbine blades serve as thrust-generating propellers to provide a second pulling force through the tether to pull the vehicle