Abstract: Example methods and systems for providing information to a pilot of a receiver aircraft during a refueling operation are described. The refueling operation includes a tanker aircraft with a hose for supplying fuel to the receiver aircraft and a refueling coupler coupled to an end of the hose. One example method includes, receiving at a first transceiver located at the receiver aircraft refueling information from a second transceiver located at the tanker aircraft, receiving from a vision system located at the receiver aircraft image information indicative of the hose and the refueling coupler, and displaying, on a head up display (HUD) of the pilot of the receiver aircraft a visual representation of one or more of the refueling information and the image information.

Abstract: An example indication system for use with a refueling system including a hose for supplying fuel from a tanker aircraft to a receiver aircraft and a refueling coupler coupled to an end of the hose is described. The indication system includes a first transceiver located at the refueling coupler and configured to receive refueling information from a second transceiver located at the tanker aircraft, a plurality of light sources located at the refueling coupler, and a processor in communication with the first transceiver to receive the refueling information, and in communication with the plurality of light sources to operate the plurality of light sources based on the refueling information.

Abstract: Example methods and systems for providing information to a pilot of a receiver aircraft during a refueling operation are described. The refueling operation includes a tanker aircraft with a hose for supplying fuel to the receiver aircraft and a refueling coupler coupled to an end of the hose. One example method includes, receiving at a first transceiver located at the receiver aircraft refueling information from a second transceiver located at the tanker aircraft, receiving from a vision system located at the receiver aircraft image information indicative of the hose and the refueling coupler, and displaying, on a head up display (HUD) of the pilot of the receiver aircraft a visual representation of one or more of the refueling information and the image information.

Abstract: Example methods and systems for providing information to a pilot of a receiver aircraft during a refueling operation are described. The refueling operation includes a tanker aircraft with a hose for supplying fuel to the receiver aircraft and a refueling coupler coupled to an end of the hose. One example method includes, receiving at a first transceiver located at the receiver aircraft refueling information from a second transceiver located at the tanker aircraft, receiving from a vision system located at the receiver aircraft image information indicative of the hose and the refueling coupler, and displaying, on a head up display (HUD) of the pilot of the receiver aircraft a visual representation of one or more of the refueling information and the image information.

Abstract: Example methods and systems for providing information to a pilot of a receiver aircraft during a refueling operation are described. The refueling operation includes a tanker aircraft with a hose for supplying fuel to the receiver aircraft and a refueling coupler coupled to an end of the hose. One example method includes, receiving at a first transceiver located at the receiver aircraft refueling information from a second transceiver located at the tanker aircraft, receiving from a vision system located at the receiver aircraft image information indicative of the hose and the refueling coupler, and displaying, on a head up display (HUD) of the pilot of the receiver aircraft a visual representation of one or more of the refueling information and the image information.

Abstract: An example indication system for use with a refueling system including a hose for supplying fuel from a tanker aircraft to a receiver aircraft and a refueling coupler coupled to an end of the hose is described. The indication system includes a first transceiver located at the refueling coupler and configured to receive refueling information from a second transceiver located at the tanker aircraft, a plurality of light sources located at the refueling coupler, and a processor in communication with the first transceiver to receive the refueling information, and in communication with the plurality of light sources to operate the plurality of light sources based on the refueling information.