In various embodiments, specialized vehicle launch systems and methods are provided to enable personnel to launch and operate one or more UAVs from the safety of a vehicle or other mobile location. In various embodiments, a launch system comprises a launch device and an operator terminal. The launch device is adapted to be mounted on an exterior surface of a vehicle and is communicably coupled to the operator terminal, which is operable from the interior of the vehicle. The vehicle launch system allows an operator to control one or more UAVs from inside the vehicle, without requiring the operator to step outside of the vehicle to interact with the UAV or launch device.

A system for virtually experiencing an aircraft includes a trailer, an aircraft fuselage, a cabin module, a head mounted display, and a controller. The aircraft fuselage is disposed in the trailer and defines an interior with a first portion and a second portion. The first portion is substantially unfurnished. The cabin module is disposed in the second portion and includes furnishings. The head mounted display is configured for movement within the interior. The controller is configured for generating a virtual aircraft interior based on a position and an orientation of the head mounted display relative to the interior of the aircraft fuselage and for controlling the head mounted display to display the virtual aircraft interior.

Disclosed are unmanned aerial vehicle (UAV) facilities suitable for use by both emergency and non-emergency UAVs. The facilities comprise a housing having first and second moveable platforms. A cover is arranged above the second moveable platform. A drive system operates the first and second moveable platforms and the cover.

Disclosed are unmanned aerial vehicle (UAV) facilities suitable for use by both emergency and non-emergency UAVs. The facilities comprise a housing having first and second moveable platforms. A cover is arranged above the second moveable platform. A drive system operates the first and second moveable platforms and the cover.

A portable case for an unmanned aerial vehicle (UAV) and a system including a portable case for UAV and an adapter for coupling the portable case to a vehicle are disclosed. An example system may include an exterior attachment disposed on an exterior of a vehicle, an adapter configured to couple a portable case for an UAV to the exterior attachment, and a moveable cover connected to the vehicle and configured to cover the portable case when the portable case is coupled to the vehicle. An example portable case may comprise a landing pad for the UAV, a bottom portion having the landing pad and configured to connect to the exterior attachment via the adapter, and a removable upper portion configured to be connected to the bottom portion when the bottom portion is disconnected from the at least one exterior attachment.

A portable case for an unmanned aerial vehicle (UAV) and a system including a portable case for UAV and an adapter for coupling the portable case to a vehicle are disclosed. An example system may include an exterior attachment disposed on an exterior of a vehicle, an adapter configured to couple a portable case for an UAV to the exterior attachment, and a moveable cover connected to the vehicle and configured to cover the portable case when the portable case is coupled to the vehicle. An example portable case may comprise a landing pad for the UAV, a bottom portion having the landing pad and configured to connect to the exterior attachment via the adapter, and a removable upper portion configured to be connected to the bottom portion when the bottom portion is disconnected from the at least one exterior attachment.

A drone landing apparatus may include: a trunk door configured to open or close a trunk of a vehicle; a drone housing contained in the trunk, and configured to provide a space in which a drone is housed; a rotator mounted on the trunk door, and configured to rotate the drone housing according to an opening angle of the trunk door; and a moving platform appearing from the drone housing or disappearing into the drone housing, and having the drone seated thereon.

Systems, methods, and computer-readable media are disclosed for drone vehicle integration and controls. A vehicle device for controlling an unmanned aerial vehicle (UAV) may receive an input indicating a request to deploy the UAV from a vehicle. The vehicle device may determine that one or more deployment conditions are satisfied. The vehicle device may cause deployment of the UAV. The vehicle device may determine a control command for the UAV and a vehicle instruction associated with operating the UAV. The vehicle device may determine that the vehicle instruction has been satisfied, and may send the control command once the vehicle instruction is satisfied.

Systems, methods, and computer-readable media are disclosed for drone vehicle integration and controls. A vehicle device for controlling an unmanned aerial vehicle (UAV) may receive an input indicating a request to deploy the UAV from a vehicle. The vehicle device may determine that one or more deployment conditions are satisfied. The vehicle device may cause deployment of the UAV. The vehicle device may determine a control command for the UAV and a vehicle instruction associated with operating the UAV. The vehicle device may determine that the vehicle instruction has been satisfied, and may send the control command once the vehicle instruction is satisfied.

A wireless remote controlled rotorcraft tug assembly and method of maneuvering a rotorcraft positions a rotorcraft, of the type having skids, through use of a remote controlled low-profile tug vehicle that maneuvers in a tight 360 motion to maneuver the rotorcraft to a desired location, and operates multiple arms to raise, lower, and support the rotorcraft. A forward support arm and at least one lever arm are selectively movable through hydraulic or electrical means to engage the undercarriage of the fuselage for raising, lowering, and supporting the rotorcraft. A lateral arm connects to the skids from free ends to raise and lower the rotorcraft by the skids. A motor advances the tug vehicle by powering a drive wheel. A guide wheel attaches to a steering mechanism and enables 360 turns and precise maneuverability. A radio receiver and transmitter work to remotely control the motor and the arm control subassembly.