Abstract: An authorization system includes a controller of an external computing device communicatively connected to an unmanned aerial vehicle (UAV). The controller obtains a mission kit that includes software for controlling a piece of equipment configured to be assembled on the UAV. The controller receives a license that is associated with a user and determines, based on the license, whether the piece of equipment is authorized for operation on the UAV as controlled by the user. Responsive to determining that the piece of equipment is authorized, the controller initiates transmission of at least some of the software of the mission kit to the UAV for installation by the UAV to allow the user to operate the piece of equipment.

Abstract: An authorization system includes a controller of an external computing device communicatively connected to an unmanned aerial vehicle (UAV). The controller obtains a mission kit that includes software for controlling a piece of equipment configured to be assembled on the UAV. The controller receives a license that is associated with a user and determines, based on the license, whether the piece of equipment is authorized for operation on the UAV as controlled by the user. Responsive to determining that the piece of equipment is authorized, the controller initiates transmission of at least some of the software of the mission kit to the UAV for installation by the UAV to allow the user to operate the piece of equipment.

Abstract: An aircraft includes a fuselage module and at least two vertical lift rotor modules supporting at least four rotor assemblies. Each rotor assembly is supported by a rotor boom having at least one boom free end and a boom mounting portion. Each rotor assembly has at least one vertical lift rotor mounted on the boom free end. Each boom mounting portion is removably couplable to the fuselage module. The vertical lift rotor modules are configured such that when coupled to the fuselage module, a pair of the rotor assemblies are located on each of laterally opposite sides of the fuselage module, and the rotor assemblies of each pair are respectively located forward of and aft of a wing center portion. A pair of wings are configured to be removably couplable to the wing center portion. The aircraft includes a forward thrust module removably couplable to the fuselage body.

Abstract: An aircraft includes a fuselage module and at least two vertical lift rotor modules supporting at least four rotor assemblies. Each rotor assembly is supported by a rotor boom having at least one boom free end and a boom mounting portion. Each rotor assembly has at least one vertical lift rotor mounted on the boom free end. Each boom mounting portion is removably couplable to the fuselage module. The vertical lift rotor modules are configured such that when coupled to the fuselage module, a pair of the rotor assemblies are located on each of laterally opposite sides of the fuselage module, and the rotor assemblies of each pair are respectively located forward of and aft of a wing center portion. A pair of wings are configured to be removably couplable to the wing center portion. The aircraft includes a forward thrust module removably couplable to the fuselage body.