A server device transmits an instruction for causing a plurality of flying bodies to perform flight operation to the flying bodies. The flight operation includes a step in which a first flying body urges a penetrating tool toward an object placed in a predetermined space and flies out of the predetermined space while holding a first part and a second part of a string member attached to the penetrating tool, the first part having penetrated the object and the second part not having penetrated the object, a step in which a second flying body receives either the first or second part from the first flying body, and a step in which the first and second flying bodies transport the object while towing the object with the string member as the first and second flying bodies fly while respectively holding one or the other of the first and second parts.

A method for determining a route for a drone to deliver a package from an origin to a destination using vehicles that are not actively participating in a delivery of a package; a method for delivering the package from the origin to the destination using the drone in accordance with the route; a method for determining a route for delivering a package from an origin to a destination using drones and vehicles that are not actively participating in a delivery of the package; a method for delivering the package from the origin to the destination using the drones and vehicles in accordance with the route; a vehicle-associated package repository, for retaining packages deposited and collect by a drone, to be transported by a vehicle; and a vehicle-transported container including the vehicle-associated package repository.

An autonomous cargo container retrieval and delivery system locates a select cargo container and maneuvers an unmanned aerial vehicle proximate to the container for retrieval. The vehicle positions itself to engage the cargo container using a grasping mechanism, and, responsive to engaging the cargo container, retracts the cargo container toward the vehicle. As the cargo container is retracted toward the vehicle, weight sensors within the retrieval mechanism sense the weight and the weight distribution of the cargo container, and, can modify the cargo container's location on the vehicle to optimize vehicle flight operations or replace the container on the ground and alert the operator that the cargo container is too heavy or has an improper weight distribution. Upon mating the cargo container with the vehicle, a coupling mechanism latches or secures the cargo container to the vehicle for further flight and/or ground operations.

The article transfer system S selects an article transfer candidate on the basis of first sensing information obtained from first sensing performed by the unmanned aerial vehicle in flight, performs a movement control of the unmanned ground vehicle on the basis of position information of the selected article transfer candidate, and determines an article transfer place with reference to the selected article transfer candidate on the basis of second sensing information obtained from second sensing performed by the unmanned ground vehicle.

Methods, systems, and apparatus, including computer programs encoded on computer storage media, for a distributed system architecture for unmanned air vehicles. One of the methods includes obtaining information identifying flight information of a UAV, with the flight information including flight phase information or a contingency condition associated with a flight critical module included in the UAV. The obtained information is analyzed, and one or more first payload modules are determined to enter a modified power state. Requests to enter the modified power state are caused to be transmitted to each determined payload module in the one or more first payload modules.

An unmanned vehicle (UV) navigation system is provided. The UV navigation system comprises a processor, a communication interface for communicating with a remote station, and a non-transitory memory device storing machine-readable instructions that, when executed by the processor, causes the processor to navigate the UV. The processor is configured to receive data from sensors, camera or data line for UV processor analysis, determine that a link-free trigger event has occurred, and autonomously navigate the UV in response to the trigger event.

A multiple hoist system is used with an unmanned aerial vehicle (UAV) for delivering parcels. An example of the multiple hoist system comprises two or more hoists that are independently operable, meaning that a first hoist can lower or raise a first line independently of using a second hoist to raise or lower a second line. The hoists can independently raise and lower their associated lines to allow the UAV to deliver multiple parcels to multiple delivery locations, or the hoists can synchronously raise and lower the associated lines together so that larger parcels can be delivered using the UAV. The hoists can be comprised within a body of the multiple hoist system. The body can further include a securing device for releasably securing the multiple hoist system to the UAV.

A system includes a higher unmanned multicopter, a lower unmanned multicopter, and a flexible connector. The flexible connector connects the higher unmanned multicopter and the lower unmanned multicopter. The VTM system is configured to carry a payload, including by having the higher unmanned multicopter fly above the lower unmanned multicopter with the flexible connector taut such that both the higher unmanned multicopter and the lower unmanned multicopter contribute to carrying the payload.

An aerial vehicle has a loading section whereon a payload and the like can be loaded. The aerial vehicle is capable of traveling at least forward and backward, is provided with lift generation sections, arm sections for holding the lift generation sections, a loading section disposed on the arm sections and positioned posterior to the center of gravity of the aerial vehicle, and a maintaining means for maintaining the aerial vehicle at least in the horizontal attitude, and the loading section has a first connection part for maintaining a loaded object at least in the horizontal attitude. On the basis of the above mentioned, the payload can be prevented from entering slipstream regions created by propellers, improving flight efficiency.

An airplane emergency escape drone is shown and described. The airplane emergency escape drone includes a life support system secured within a housing with a compressed air tank that controls the amount of oxygen from an oxygen tank and air from an air tank released into the housing. The airplane emergency escape drone also includes an inflatable floatation device secured to the housing. The airplane emergency escape drone also includes propellers having safety grates underneath the propellers. The airplane emergency escape drone also includes a CPU that is in connection with a video control system that includes a video input component and a signal transmitter.