Systems, devices, and methods for a ground support system for an unmanned aerial vehicle (UAV) including: at least one handling fixture, where each handling fixture is configured to support at least one wing panel of the UAV; and at least one dolly, where each dolly is configured to receive at least one landing pod of the UAV, and where each landing pod supports at least one wing panel of the UAV; where the at least one handling fixture and the at least one dolly are configured to move and rotate two or more wing panels to align the two or more wing panels with each other for assembly of the UAV; and where the at least one dolly further allows for transportation of the UAV over uneven terrain.

A UAV landing platform having movable covers to securely store/maintain/charge a UAV. The UAV may be launched from the landing platform, and the landing platform can have visual indicators to guide the landing of the UAV back onto the landing platform. There can be an optional mechanism to self-adjust/self-level the landing surface such that a UAV can safely land onto the landing platform even when the landing platform is on a traveling vehicle.

Method for inspecting and/or manipulating a beam at a lower side of a roof or deck, the beam including a strip, the method comprising the steps of:

providing an unmanned aerial vehicle, UAV, wherein the UAV comprises a body, a number of rotors, a first arm; and an inspection and/or manipulation tool; while the first arm is in the first position, flying the UAV towards the beam; when the UAV contacts the beam, moving the first arm from the first position to the second position such that the end of the first arm is moved to a position vertically above the strip; reduce the propulsion force until the UAV hangs from the beam with the end of the arm in contact with and supported by the strip; and inspecting and/or manipulating the beam, using the inspection and/or manipulation tool, while the UAV hangs from the beam.

Multi-rotor rotorcraft (10) comprise a fuselage (12), and at least four rotor assemblies (14) operatively supported by and spaced-around the fuselage (12). Each of the at least four rotor assemblies (14) defines a spin volume (24) and a spin diameter (26). Some multi-rotor rotorcraft (10) further comprise at least one rotor guard (50) that is fixed relative to the fuselage (12), that borders the spin volume (24) of at least one of the at least four rotor assemblies (14), and that is configured to provide a visual indication of the spin volume (24) of the at least one of the at least four rotor assemblies (14). Various configurations of rotor guards (50) are disclosed.

A flexible landing gear system for a vertical take-off and landing (VTOL) aircraft is disclosed. The flexible landing gear system may comprise a mounting bracket, a plurality of flexible supports, and plurality of surface contactors. The mounting bracket may be configured to couple to the VTOL aircraft. Each of the plurality of flexible supports comprising a proximal end and a distal end. The plurality of flexible supports may be coupled to the mounting bracket at a proximal end. A surface contactor may be positioned at the distal end of each of the plurality of flexible supports. The low-friction contactor may be a lightweight spherical ball, while the flexible support may be a flexible semi-rigid wire comprising a tempered high-carbon steel.

A UAV landing platform having movable covers to securely store/maintain/charge a UAV. The UAV may be launched from the landing platform, and the landing platform can have visual indicators to guide the landing of the UAV back onto the landing platform. There can be an optional mechanism to self-adjust/self-level the landing surface such that a UAV can safely land onto the landing platform even when the landing platform is on a traveling vehicle.

A payload support frame is adapted to suspend a payload from an unmanned aerial vehicle (UAV) during flight. The frame comprises at least one elongated rigid segment, at least one upper flexible segment at an upper end of the rigid segment, and at least one lower flexible segment at a lower end of the rigid segment. One or more of (a) the at least one rigid segment, (b) the at least one upper flexible segment, or (c) the at least one lower flexible segment comprise a dielectric material. The upper flexible segment is adapted to be selectively attachable, directly or indirectly, to the UAV. The lower flexible segment is adapted to be selectively attachable, directly or indirectly, to the payload.

A combination payload retrieval and package pickup apparatus having a base, an autoloader assembly mounted to the base including a payload holder configured to hold a payload for retrieval by a UAV, a channel coupled to the payload holder and configured to direct a payload coupling apparatus to the payload holder, a package receptacle housing having package receptacles configured to house a package to be picked up, wherein each of the package receptacles includes a locking feature to secure a package to be picked up in the package receptacle, wherein the locking feature is configured to be unlocked upon receipt of a first access code to allow access to an interior of the package receptacle to allow a package to be placed into, or removed from, the package receptacle.

A combination payload retrieval and package pickup apparatus having a base, an autoloader assembly mounted to the base including a payload holder configured to hold a payload for retrieval by a UAV, a channel coupled to the payload holder and configured to direct a payload coupling apparatus to the payload holder, a package receptacle housing having package receptacles configured to house a package to be picked up, wherein each of the package receptacles includes a locking feature to secure a package to be picked up in the package receptacle, wherein the locking feature is configured to be unlocked upon receipt of a first access code to allow access to an interior of the package receptacle to allow a package to be placed into, or removed from, the package receptacle.

A aerial drone deployed NDE scanner test unit (12) has a yoke to which four sets of offset pins (294, 354) pivotally secure a sensor probe (232) in a configuration for rotating about the X-axis and the Y-axis with constrained rotation. Each set of the offset pins (294, 354) are spaced apart, with the ends closest to the terminal ends of the sensor probe (232) and an EUT (26) being more closely spaced than opposite ends of the offset pins (294, 354). The NDE scanner (16) is deployed from an aerial drone (14) with a cable (18) and an umbilical (20) connecting there-between. The cable (18) selectively secures the NDE scanner (16) to the aerial drone (14) and the umbilical (20) provides data and fluid connections. The NDE scanner (16) has a stand-off mechanism (118) which is selectively operated to engage and disengage the magnetic wheels (94) of the NDE scanner (16) from a metal surface of the EUT (26).