Abstract: Disclosed are systems, methods, computer program products, and devices for fully- or semi-autonomously managing the launch and movement of an unmanned vehicle or fleet of unmanned vehicles. In some aspects, a system includes a centralized data management system in communication over a network (e.g., public or private network) with a coded (fleet of) unmanned vehicle(s) and client devices that are distributed throughout areas of interest and operable by remote users to remotely program instructions for controlling one or more activities or tasks of the unmanned vehicle with complete secrecy of the instructions and anonymity of the remote user between client devices.

Abstract: Disclosed are specialized airframe structures for mission-adaptable unmanned aerial vehicles (UAVs) that are fabricated by rapid, low-cost additive manufacturing techniques. In some embodiments, an integral fastening system for a mission-adaptable aerial vehicle includes a first airframe section, a second airframe section, and a bayonet mount system that comprises one or more passageways produced on a first end region of the first airframe section to include a first channel and second channel, and one or more protrusions produced on a second end region of the second airframe section, such that, when the first and second airframe sections being assembled, the one or more protrusions are first aligned with an entry region of the first channel to be translated and then aligned with the second channel of the one or more passageways to be rotated to securely connect the first and second airframe sections together.

Abstract: Disclosed are devices, systems and methods for mission-adaptable aerial vehicle. In some aspects, a mission-adaptable aerial vehicle includes a configuration having swappable, manipulatable, and interchangeable sections and components connectable by a connection and fastening system able to be modified by an end-user in the field. In some embodiments, a mission-adaptable aerial vehicle can be configured to include a main center body extending along a longitudinal direction, a wing with a lateral cross-sectional airfoil shape, and/or stabilizer and control surface structures with corresponding cross-sectional airfoil shapes.

Abstract: Disclosed are devices, systems and methods for mission-adaptable aerial vehicle. In some aspects, a mission-adaptable aerial vehicle includes a configuration having swappable, manipulatable, and interchangeable sections and components connectable by a connection and fastening system able to be modified by an end-user in the field. In some embodiments, a mission-adaptable aerial vehicle can be configured to include a main center body extending along a longitudinal direction, a wing with a lateral cross-sectional airfoil shape, and/or stabilizer and control surface structures with corresponding cross-sectional airfoil shapes.

Abstract: Disclosed are devices, systems and methods for mission-adaptable aerial vehicle. In some aspects, a mission-adaptable aerial vehicle includes a configuration having swappable, manipulatable, and interchangeable sections and components connectable by a connection and fastening system able to be modified by an end-user in the field. In some embodiments, a mission-adaptable aerial vehicle can be configured to include a main center body extending along a longitudinal direction, a wing with a lateral cross-sectional airfoil shape, and/or stabilizer and control surface structures with corresponding cross-sectional airfoil shapes.

Abstract: Disclosed are devices, systems and methods for mission-adaptable aerial vehicle. In some aspects, a mission-adaptable aerial vehicle includes a configuration having swappable, manipulatable, and interchangeable sections and components connectable by a connection and fastening system able to be modified by an end-user in the field. In some embodiments, a mission-adaptable aerial vehicle can be configured to include a main center body extending along a longitudinal direction, a wing with a lateral cross-sectional airfoil shape, and/or stabilizer and control surface structures with corresponding cross-sectional airfoil shapes.

Abstract: Disclosed are devices, systems and methods for mission-adaptable aerial vehicle. In some aspects, a mission-adaptable aerial vehicle includes a configuration having swappable, manipulatable, and interchangeable sections and components connectable by a connection and fastening system able to be modified by an end-user in the field. In some embodiments, a mission-adaptable aerial vehicle can be configured to include a main center body extending along a longitudinal direction, a wing with a lateral cross-sectional airfoil shape, and/or stabilizer and control surface structures with corresponding cross-sectional airfoil shapes.