An unmanned autonomous vehicle is provided and includes at least one propulsion device, at least one image capture device, at least one adjusting member to adjust an tilt angle of the image capture device and is configured to receive, from a control device, a capturing instruction to capture at least one image, acquire angle information indicating a tilt angle of the image capture device, and control, in a case where the capturing instruction is received, the propulsion device so that the image capture device captures at least one image at an altitude which is determined based on the acquired angle information.

An unmanned autonomous vehicle is provided and includes at least one propulsion device, at least one image capture device, at least one adjusting member to adjust an tilt angle of the image capture device and is configured to receive, from a control device, a capturing instruction to capture at least one image, acquire angle information indicating a tilt angle of the image capture device, and control, in a case where the capturing instruction is received, the propulsion device so that the image capture device captures at least one image at an altitude which is determined based on the acquired angle information.

A flight-capable imaging system includes a set of parallel rails, a power source mounted to the set of parallel rails, an imaging device mounted to the set of parallel rails, an aerial vehicle body mounted to the set of parallel rails, a set of aerial vehicle arms attached to the aerial vehicle body that each include a set of propellers and a motor configured to turn the set of propellers to enable flight of the flight-capable imaging system, and at least one processing module configured to control the flight of the of the flight-capable imaging system based on controlling a motor speed of the motor of each of the set of aerial vehicle arms.

A compact directed energy system is disclosed that is configured to generate directed energy beams. The compact directed energy system includes a radio frequency system configured to provide a directed energy beam in a frequency range between 500 MHz to 20 Ghz.

Accessory port systems and methods are provided. In one example, an unmanned aerial vehicle (UAV) includes an accessory port configured to interchangeably attach a plurality of accessory devices to the UAV. The accessory port may have a mechanical interface configured to engage with one of the accessory devices. The mechanical interface may include a locking member configured to physically secure the accessory device to the accessory port. The accessory port may further include an electrical interface configured to electrically connect the accessory device to the UAV. The mechanical interface may be configured to align the accessory device relative to the electrical interface. Related devices, systems, and methods are also provided.

A field configurable autonomous vehicle includes modular elements and attachable components. The vehicle can be assembled from these modular elements and components to meet desired mission and performance characteristics without the need to purchase specially designed vehicles for each mission. The vehicle can include a module that enables the vehicle to adjust the position of the center of mass to trim the vehicle for efficient operations or to alter the stability and control parameters of the vehicle.

The present disclosure is directed to unmanned aerial vehicle (UAV) comprising a convertible body operably coupled to at least one sensor, and further configured to rotate at least about a longitudinal axis, thereby providing a full field of regard for the at least one sensor, and a plurality of arms extending laterally from the convertible body, each arm of the plurality of arms having a rotor assembly coupled thereto.

Problems to be Solved

To provide an unmanned aerial vehicle capable of achieving both of equipping a pruning structure capable of pruning trees and enhancing safety.

Solution

An unmanned aerial vehicle 2 according to the present invention includes a pruning structure 23 capable of pruning a tree; a housing structure 24 capable of housing the pruning structure 23 inside; and a state control section 212 capable of controlling the state of the pruning structure 23 between a housed state in which the pruning structure 23 is housed inside the housing structure 24 and an exposed state in which the pruning structure 23 is exposed to the outside of the housing structure 24, wherein the state control section 212 can control the state of the pruning structure 23 to the housed state on landing. The state control section 212 preferable to control the state of the pruning structure 23 to the exposed state when a distance from the unmanned aerial vehicle 2 to a target tree to be pruned equal to or shorter than the predetermined distance, and to control the state of the pruning structure 23 to the housed state when a distance from the unmanned aerial vehicle 2 to the target tree longer than the predetermined distance.

Systems and methods for operating done flights over public roadways are disclosed herein. An example method includes transmitting, by a first drone, a drone safety message, the drone safety message being received by a vehicle or a roadside infrastructure device located along a first planned flight path, determining an emergency condition for the first done, transmitting a warning message over a vehicle-to-everything communication that indicates that the first drone is experiencing the emergency condition. A connected vehicle or mobile device receives the warning message over the vehicle-to-everything communication. Determining drone operating evidence as the first drone traverses along the first planned flight path, and storing the drone operating evidence in a distributed ledger.

A shield system for an unmanned arial vehicle (AUV) is provided. The shield system includes inner shield members rigidly mounted to at least the rotor arms of the AUV and outer shield members shock mounted to the inner shield members. The shield system defines opening for sensors, payload or mechanical portions of the UAV.