Unmanned aerial vehicles (UAVs) and control thereof to assemble into flexible, dynamic structures. A UAV includes a flexible screen retractable between extended and retracted positions, connector(s) for coupling to another UAV that can pull the flexible screen from a retracted position to an extended position, and a coupling portion for coupling to connector(s) of yet another UAV to connect to and extend a flexible screen thereof. Chain(s) of coupled UAVs with extended flexible screens thereof form a structure that can change shape and size based on UAV movement. Local wireless communication with a group control UAV facilitates coordinated positioning and control of a UAV group. A group control UAV with a power supply and an electrical conducting lead can power UAVs of a group while it and they are in-flight, and can perform real-time management of the group UAVs in forming and maintaining a desired shape of the structure.

A method includes providing an image to a feature extraction model to generate feature data. The image depicts a portion of a first device and a portion of a second device. The feature data includes coordinates representing key points of each of the first and second devices depicted in the image. The method also includes obtaining position data indicating a position in 3D space of a connector of the first device. The method further includes providing the feature data and the position data to a trained autonomous agent to generate a proposed maneuver to mate the connector with a connector of the second device.

Aspects of the disclosure provide solutions for automated air-to-air refueling (A3R) and assisted air-to-air refueling. Examples include: receiving a video frame; generating, from the video frame, a plurality of images having differing decreasing resolutions; detecting, within each of the plurality of images, a set of aircraft keypoints for an aircraft to be refueled; merging the sets of aircraft keypoints into a set of merged aircraft keypoints; based on at least the merged aircraft keypoints, determining a position of a fuel receptacle on the aircraft; and determining a position of a boom tip of an aerial refueling boom. Some examples include, based on at least the position of the fuel receptacle and the position of the boom tip, controlling the aerial refueling boom to engage the fuel receptacle, and for some examples, the video frame is monocular (e.g., provided by a single camera).

A system for transferring a fluid from a first spacecraft to a second spacecraft. The first spacecraft includes a fluid transfer system comprising: a pressurant supply system, a first fluid tank to store a fluid to be transferred, one or more transfer feedlines to provide fluidic connection between the first fluid tank and the second spacecraft, a connector for connecting the first spacecraft to the second spacecraft, an accumulator tank comprising a first portion connected to the pressurant supply system, a second portion configured in fluidic communication with the one or more transfer feedlines, and a flexible separator to separate the first portion and the second portion. The pressurant supply system supplies pressurant gas to the first fluid tank for pressurising the first fluid tank and to supply pressurant gas to the first portion of the accumulator tank for pressurising the first portion of the accumulator tank.

An en route fluid transmitting apparatus for transmitting a fluid from a transmitting entity to a probe of a receiving vehicle includes a funnel, a hose and a thrust producing device. Thrust producing device includes a main body that is rigidly attached to the funnel, and at least two rotors that are connected to the main body for producing thrust. The thrust producing device is adapted to move the funnel freely in any direction to a predetermined position relative to the probe where the funnel engages with the probe.

An en route fluid transmitting apparatus for transmitting a fluid from a transmitting entity to a probe of a receiving vehicle includes a funnel, a hose and a thrust producing device. Thrust producing device includes a main body that is rigidly attached to the funnel, and at least two rotors that are connected to the main body for producing thrust. The thrust producing device is adapted to move the funnel freely in any direction to a predetermined position relative to the probe where the funnel engages with the probe.

A boom pod with an adaptable user interface automatically reconfigures based on operation phase. Elements of the user interface may also be manually reconfigured based on operator preference. Operator reconfigurations may be recorded for use during similar phases in subsequent operations. A controller automatically records system status during a refueling operation and prepares a digital log entry. Portions of the use interface are dedicated to augmented displays to assist the operator at any given operational phase.

A variety of refueling devices, systems and methods are disclosed for use in in-flight refueling. In one example one such device is towed by a tanker aircraft via a fuel hose at least during in-flight refueling, and has a boom member with a boom axis. The boom member enables fuel to be transferred from the fuel hose to a receiver aircraft along the boom axis during in-flight refueling. The device maintains a desired non-zero angular disposition between the boom axis and a forward direction at least when the refueling device is towed by the tanker aircraft in the forward direction via the fuel hose.

A variety of refueling devices, systems and methods are disclosed for use in in-flight refueling. In one example one such device is towed by a tanker aircraft via a fuel hose at least during in-flight refueling, and has a boom member with a boom axis. The boom member enables fuel to be transferred from the fuel hose to a receiver aircraft along the boom axis during in-flight refueling. The device maintains a desired non-zero angular disposition between the boom axis and a forward direction at least when the refueling device is towed by the tanker aircraft in the forward direction via the fuel hose.

The present disclosure relates to imaging processing devices, aerial refueling aircraft, and methods relating to the processing of images. An example imaging processing device includes a programmable circuit, such as a field-programmable gate array (FPGA), that is reprogrammed based on selected circuit data so as to construct a circuit configured to provide image processing on at least one image. The image processing includes receiving the at least one image. The image processing also includes adjusting the at least one image, to provide at least one adjusted image. Adjusting the at least one image includes applying: a local adaptive histogram equalization filter, a global gamma correction filter, and a local contrast filter.