Abstract: A method for performing automated refueling operations includes receiving a two-dimensional (2D) image of a device associated with in-flight refueling operations between a receiver aircraft and a tanker aircraft, identifying keypoints on the device in the 2D image, projecting the keypoints to three-dimensional (3D) space to produce 3D keypoints, comparing the 3D keypoints to a previously stored 3D model of the device to produce a confidence value, and automatically controlling the refueling operations in response to the confidence value.

Abstract: Disclosed herein is methods, systems, and aircraft for performing refueling operations. A method of controlling pilot director lights includes generating, using a camera of a tanker aircraft, a two-dimensional (2D) image of a receiver aircraft and a refueling boom of the tanker aircraft, determining a 2D position of a boom receptacle on the receiver aircraft within the 2D image, determining a three-dimensional (3D) position of the boom receptacle with regard to an origin location of the camera of the tanker aircraft, moving the 3D position of the boom receptacle to have a boom pivot origin to produce a moved 3D position of the boom receptacle, and controlling one or more pilot director lights based on the moved 3D position.

Abstract: A small thin display unit that can be installed in the flight deck for displaying only flight crew-selected tactical information needed for the task at hand. The flight crew can select the tactical information to be displayed by means of any conventional user interface. Whenever the flight crew selects tactical information for display, the user interface sends a corresponding request for tactical information to a computer system. The computer system processes the request, including periodically retrieving measured current values or computing current values for the requested tactical parameters and returning those current tactical parameter values to the display unit for display.

Abstract: A small thin display unit that can be installed in the flight deck for displaying only flight crew-selected tactical information needed for the task at hand. The flight crew can select the tactical information to be displayed by means of any conventional user interface. Whenever the flight crew selects tactical information for display, the user interface sends a corresponding request for tactical information to a computer system. The computer system processes the request, including periodically retrieving measured current values or computing current values for the requested tactical parameters and returning those current tactical parameter values to the display unit for display.

Abstract: A small thin display unit that can be installed in the flight deck for displaying only flight crew-selected tactical information needed for the task at hand. The flight crew can select the tactical information to be displayed by means of any conventional user interface. Whenever the flight crew selects tactical information for display, the user interface sends a corresponding request for tactical information to a computer system. The computer system processes the request, including periodically retrieving measured current values or computing current values for the requested tactical parameters and returning those current tactical parameter values to the display unit for display.