B64U10/00

CONTROL DEVICE, PROGRAM, SYSTEM, AND METHOD
20230308614 · 2023-09-28 ·

Provided is a control device including a location information reception unit which receives, via a communication device, location information of a user terminal from the terminal in a wireless communication area, a detection device control unit which controls a detection device of a flying object to detect a state of a region including a location indicated by the location information, a detection information reception unit which receives, via the communication device, detection information indicating the state, an unmanned aerial vehicle control unit which controls an unmanned aerial vehicle to capture an image around the location by an image capturing unit of the vehicle based on the detection information, a captured image reception unit which receives a captured image captured by the image capturing unit from the vehicle, and a rescue method decision unit which decides a rescue method of rescuing a user of the terminal based on the image.

Propulsion flow path duct systems and methods

A flow path duct system for a propulsion system of an aircraft includes a base defining a flow surface. The base has an internal surface and an external surface. A plurality of perforations are formed through the base between the internal surface and the external surface. A plurality of supports define a plurality of cavities. The plurality of supports extend outwardly from the external surface of the of the base. One or more of the plurality of cavities are in fluid communication with the one or more of the plurality of perforations. A backing surface is secured to the plurality of supports. The plurality of supports are disposed between the base and the backing surface. The one or more of the plurality of cavities are in fluid communication with an internal volume defined by the internal surface of the base through the one or more of the plurality of perforations. The base, the plurality of supports, and the backing surface can be integrally formed together as a monolithic, load-bearing structure.

Method, device and system for presenting operation information of a mobile platform

A method for presenting operational information of a mobile platform includes collecting diagnostic data and travel route data associated with an operation of the mobile platform, and integrating the travel route data with the diagnostic data for presentation. The diagnostic data includes at least one of platform diagnostic data or remote control data. The remote control data is generated by a remote controller associated with the mobile platform or generated by a computer device.

Vehicle docking systems, payload transfer systems, and related methods
11174027 · 2021-11-16 · ·

Vehicle docking systems, payload transfer systems, and related methods. A vehicle docking system includes a vehicle with a plurality of docking insert units and a docking platform with a plurality of docking receptor units. Each docking receptor unit is configured to transition between an unlocked configuration and a locked configuration. A method of utilizing a vehicle docking system includes bringing a vehicle to a docked position on a docking platform and securing the vehicle in the docked position. The docking platform includes a plurality of docking receptor units and the vehicle includes a plurality of docking insert units, each docking receptor unit configured to receive a corresponding docking insert unit. The securing the vehicle in the docked position includes transitioning each docking receptor unit from an unlocked configuration to a locked configuration. A payload transfer system includes a payload engagement system and a vehicle docking system.

Unmanned aerial vehicle with enhanced cargo storage

System and method for loading cargo onto an unmanned aerial vehicle (UAV). One embodiment is a cargo pod for an unmanned aerial vehicle (UAV). The cargo pod includes a hollow body that forms a section of a fuselage of the UAV, and further includes a latching mechanism that releasably secures the hollow body with the fuselage of the UAV.

System and method for thermal control during delivery of a medication package

A method for controlling an autonomous unmanned aerial vehicle for delivery of a medication package includes determining a thermal control period for the medication package. The method also includes identifying a delivery location corresponding to the medication package. The method also includes identifying at least one environmental characteristic of an environment that includes a delivery three-dimensional flight path between a starting location and the delivery location, wherein the at least one environmental characteristic indicates an actual weather value at the delivery location. The method also includes determining whether to deliver the medication package based on the thermal control period and the at least one environmental characteristic, using the unmanned aerial vehicle.

System and method for thermal control during delivery of a medication package

A method for controlling an autonomous unmanned aerial vehicle for delivery of a medication package includes determining a thermal control period for the medication package. The method also includes identifying a delivery location corresponding to the medication package. The method also includes identifying at least one environmental characteristic of an environment that includes a delivery three-dimensional flight path between a starting location and the delivery location, wherein the at least one environmental characteristic indicates an actual weather value at the delivery location. The method also includes determining whether to deliver the medication package based on the thermal control period and the at least one environmental characteristic, using the unmanned aerial vehicle.

INSURANCE UNDERWRITING AND RE-UNDERWRITING IMPLEMENTING UNMANNED AERIAL VEHICLES (UAVS)

Unmanned aerial vehicles (UAVs) may facilitate insurance-related tasks. UAVs may actively be dispatched to an area surrounding a property, and collect data related to property. A location for an inspection of a property to be conducted by a UAV may be received, and one or more images depicting a view of the location may be displayed via a user interface. Additionally, a geofence boundary may be determined based on an area corresponding to a property boundary, where the geofence boundary represents a geospatial boundary in which to limit flight of the UAV. Furthermore, a navigation route may be determined which corresponds to the geofence boundary for inspection of the property by the UAV, the navigation route having waypoints, each waypoint indicating a location for the UAV to obtain drone data. The UAV may be directed around the property using the determined navigation route.

Quick disassembling structure and unmanned aerial vehicle

A disassembling structure includes a first connecting piece, a second connecting piece and a guide and positioning piece; the guide and positioning piece is fixedly arranged on the first module; the second connecting piece is fixedly arranged on the second module; the second connecting piece and the guide and positioning piece are opposite to each other; the guide and positioning piece is attached to the outer side of the second connecting piece in a covering manner to guide and position the first module and the second module; the first connecting piece is detachably connected to the second connecting piece after passing through the guide and positioning piece.

METHOD OF CONTROLLING SAFETY OF UNMANNED AERIAL VEHICLE AND SYSTEM FOR PERFORMING THE SAME

Provided are a method of controlling safety of an Unmanned Aerial Vehicle (UAV) and a system for performing the method. The method of controlling the safety includes identifying a failure of a UAV for each of a plurality of mission performance operations of the UAV, based on status data of the UAV received in real time from the UAV and past flight performance data of a case where the UAV normally performs a mission and controlling safety of the UAV based on the failure for each of the plurality of mission performance operations and a risk level of the failure. The status data may include component operation status data of the UAV, power status data of the UAV, and communication connection status data of the UAV.