An embodiment of a disaster response system is disclosed that includes a communication and monitoring environment (CME). The CME includes an incident command infrastructure, and a communication infrastructure configured to exchange data with the incident command infrastructure. The communication infrastructure includes a network comprising a plurality of sensor assemblies that are configured to wirelessly communicate with the communication infrastructure. The sensor assemblies are configured to acquire data that includes at least one of environmental conditions, motion, position, chemical detection, and medical information. One or more of the sensors are configured to aggregate data from a subset of the plurality of sensors. The CME is configured to detect an incident based on at least the data acquired by the sensor assemblies.

Autonomous delivery drop points for delivery of an item are provided. The autonomous delivery drop points can include a proxy sensor to communicate information related to the autonomous delivery drop point to an autonomous delivery vehicle. The autonomous delivery drop points can include a delivery inlet configured to accept the item. The autonomous delivery drop points can include a storage receptacle configured to store the item until the item is retrieved by the owner of the item. The autonomous delivery drop points can include an attachment member coupled to the item. The autonomous delivery drop points can include a hook configured to couple to the attachment member to accept the item, wherein the hook comprises the proxy sensor.

Weather data is used to create and/or update a flight plan prior to and/or during flight by an unmanned aerial vehicle (UAV). The weather data may be received using sensors onboard the UAV and/or the weather data may be received from other sources, such as weather aggregators, other UAVs, other vehicles, and/or local weather stations. In some embodiments, a UAV may be prematurely grounded after initiating flight toward a destination in response to some weather conditions identified in near real-time weather data, such as heavy winds and/or heavy precipitation. In various embodiments, the UAVs may leverage air stream information included in the weather data to cause flight along with an air stream, and thereby reduce power resources used to fly to a destination.

Described is a method of delivery for cargo or goods from an aerial vehicle (mothership) to a designated ground delivery location via the use of a direct air shipping package. For example, an aerial vehicle may be an airplane or helicopter that remains at altitude with a package stowed for deployment. As the mothership travels in the vicinity of the designated location the package flight control computer (flight controller) calculates a preferred travel trajectory based upon the aerodynamic properties of the package and location relative to the designated delivery location such as a small delivery pad located on a patio of a home. When the mothership transits through a calculated release point the package disengages the mothership. As the package descends it may increase accuracy relative to the designated delivery location by altering aerodynamic properties to maintain the preferred travel trajectory and decreasing landing zone size requirements and increasing precision of delivery. To reduce the impact force at landing the designated delivery location and/or the package may contain a net, airbag, parachute or similar device to provide a suitably soft landing suitable for commercial home delivery.

In some examples, an unmanned aerial vehicle is provided. The unmanned aerial vehicle may include a propulsion device, a sensor device, and a management system. In some examples, the management system may be configured to receive human gestures via the sensor device and, in response, instruct the propulsion device to affect an adjustment to the behavior of the unmanned aerial vehicle. Human gestures may include visible gestures, audible gestures, and other gestures capable of recognition by the unmanned vehicle.

An airlift package protection (APP) airbag may protect a package (e.g., an item or a number of items) that is dropped from within a predetermined height range by an unmanned aerial vehicle (UAV). The APP airbag may at least partially surround the package and create a container for the package. In some embodiments, the APP airbag may be inflated just prior to dropping of the package from the UAV. After inflation, the APP airbag may be at least partially sealed to reduce or inhibit deflation of the APP airbag, but possibly not to completely prevent airflow from the APP airbag upon contact with the ground. The APP airbag may exhaust some air upon impact with the ground, thereby reducing a deceleration of a package contained inside of the APP airbag.

The invention relates to a method and a device for an intelligent parachute rescue system for manned and unmanned aerial vehicles (14), wherein no pyrotechnic propellants are used, but compressed air (4a) extracted from a pressure bottle (4).

A delivery container for a drone includes: an outer container (2) which is formed of an elastic material and is watertight and has a load opening (3) that opens and closes which is provided with a water stop portion (3a) to be watertight; and a cushioning portion (5) formed of an elastic material having an air chamber (6) and which is interposed between a load (B) stored inside the outer container (2) and the outer container (2) to hold the load (B) within a predetermined range inside the outer container (2). The delivery container can prevent a load to be delivered from getting damaged or wet and can easily and more reliably protect the load is provided.

In some embodiments, an aircraft includes a flying frame having an airframe, a distributed propulsion system attached to the airframe, a flight control system operably associated with the distributed propulsion system and a pod assembly selectively attachable to the flying frame. The distributed propulsion system includes a plurality of propulsion assemblies that are independently controlled by the flight control system, thereby enabling the flying frame to have a vertical takeoff and landing mode and a forward flight mode.

A system for launching a payload from an aircraft includes a magazine and a conveying mechanism. The magazine has a payload chamber at a first end of the magazine for retaining the payload and an exit port through which the payload may be launched, with the magazine configured to be disposed at or below an outer skin surface of the aircraft. The conveying mechanism includes a rotatable conveying member for contacting an outer surface of the payload when the payload is loaded into the payload chamber and for selectably rotating so as to cause the payload to be launched out of the magazine through the exit port. The system may optionally include a pivoting mechanism for pivoting the magazine between a stowed orientation and a deployed orientation, wherein the first end extends outside the outer skin surface in the deployed orientation.