Vehicles such as unmanned air vehicles that are capable of movement from an open, flight configuration to an enclosed configuration in which all major flight components can be protected by an outer shell are disclosed. In the enclosed configuration, the vehicles can take on standard geometric shapes such as a rectangular prism, sphere, cylinder, or another shape, so as to not be recognizable as an unmanned air vehicle. Embodiments of vehicles can also include interchangeable and/or wireless motor arms, motor arms which are electrically connected to the remainder of the vehicle only when in an open configuration, remote controllers removably attached to the remainder of the vehicle, and clip or other attachment mechanisms for attachment to objects such as backpacks.

A remote-controlled unmanned foldable aircraft comprises at least two motors that allow the aircraft to fly, and at least one support structure for supporting said motors; the support structure is flexible and inflatable such that the support structure can be folded and unfolded between a storage position and an operational position.

Implementations of UAV wildlife monitoring system may include a ground control station wirelessly coupled to a UAV which may include a flight controller, a first radio, a second radio, a first antenna, a second antenna, a very high frequency (VHF) radio receiver, and a computer, all operatively coupled together. The monitoring system may also include a VHF tag configured to be coupled to an animal, wherein when the VHF tag is coupled to the animal, the VHF radio receiver receives a VHF radio signal from the VHF tag using the first antenna, wherein the computer process the VHF radio signal to create the location data from the VHF radio signal, processes the location data, and sends the location data to the second radio, wherein the second radio transmits the location data into a telecommunications channel, and wherein the ground control station receives the location data from the telecommunications channel.

Devices and methods for transporting and storing a drone. Polycarbonate or material of similar resiliency is used to create a casing for the drone body. Stationary wing or retractable wing drones can be protectively coupled and attached to objects for transportation. The casing is comprised of a hood to cover the top of the drone and a carriage to receive the sides and bottom of the drone. The device allows quick access and greater versatility in storage and transportation of drones.

Vehicles such as unmanned air vehicles that are capable of movement from an open, flight configuration to an enclosed configuration in which all major flight components can be protected by an outer shell are disclosed. In the enclosed configuration, the vehicles can take on standard geometric shapes such as a rectangular prism, sphere, cylinder, or another shape, so as to not be recognizable as an unmanned air vehicle. Embodiments of vehicles can also include interchangeable and/or wireless motor arms, motor arms which are electrically connected to the remainder of the vehicle only when in an open configuration, remote controllers removably attached to the remainder of the vehicle, and clip or other attachment mechanisms for attachment to objects such as backpacks.

An unmanned flying device including a body; a first blade and at least a second blade; a coupling assembly for coupling the first blade and the at least second blade to the body, wherein the coupling assembly urges the collapsing of the first blade and the at least second blade towards the body; and wherein both the first blade and the at least second blade are rotateable about the body, and wherein the first blade and the at least second blade are deployable away from the body via rotation of the first and the at least second blades about the body.

The present application discloses an unmanned aerial vehicle. The unmanned aerial vehicle includes a support having a plurality of receiving slots; a plurality of arms attached to the support; and a plurality of propellers respectively attached to the plurality of arms. Each of the plurality of receiving slots is configured to receive one of the plurality of arms and one of the plurality of propellers attached to the one of the plurality of arms.

A smart belt system worn by a person comprising an elongated belt configured for removably coupling a plurality of devices, a GPS component coupled to the belt configured to track the geo-location and movement of the belt, a microprocessor coupled to the belt, logic instructions executing by the microprocessor configured to monitor and regulate the activities of the plurality of devices and geo-location and movement data generated by the GPS component, a memory component configured for storing the logic instructions and accessible by the microprocessor, a wireless data communications system coupled to the belt configured to wirelessly communicate with an external data communications system and the microprocessor, a power and data bus disposed within the belt and communicatively coupled to at least one of the plurality of devices, GPS component, microprocessor, memory, wireless data communications systems, and data storage component; and a data storage component coupled to the belt and accessible by the microprocessor for storing activity data of at least one of the plurality of devices and the geo-location and movement data of the belt generated by the GPS component.

Launch-controlled unmanned aerial vehicles, and associated systems and methods are disclosed. A computer-implemented method for operating an unmanned aerial vehicle in a representative embodiment includes detecting at least one parameter of a motion of the UAV as a user releases the UAV for flight. Based at least in part on the at least the one detected parameter, the method can further include establishing a flight path for the UAV, and directing the UAV to fly the flight path.

An unmanned air vehicle (UAV) having a fuselage, a foldable propulsion means to generate thrust leading to the UAV movement, a driving means to drive the propulsion means and a plurality of flight control surfaces actuators are further included. The UAV further includes at least one pair of foldable wings where the rear portion of the wings is pivotally attached to the fuselage. The wings having at least one roll control surface hinged to at least one of the foldable wings. At least a pair of tail stabilizers having ruddervators flight control surfaces hinged to the tail stabilizers. In a fully extended position or in ready to fly state position, each of the foldable wings are deployed perpendicular to one another and perpendicular to the fuselage to form an offset-x shaped wings, and in a stowed position, each of the wings are positioned parallel to one another and positioned parallel to the fuselage.