Abstract: Disclosed is an aircraft having motors operable to actuate an aircraft windshield wiper and an aircraft control surface. The aircraft includes a distributed control system having digital storage and integrated with redundant processors. The aircraft includes controller instructions stored on the digital storage operable upon execution to operate a control surface motor of the motors to actuate the control surface to impact an orientation of the aircraft and operate a windshield wiper motor of the motors to actuate the windshield wipers.

Abstract: Disclosed is an aircraft having motors operable to actuate an aircraft windshield wiper and an aircraft control surface. The aircraft includes a distributed control system having digital storage and integrated with redundant processors. The aircraft includes controller instructions stored on the digital storage operable upon execution to operate a control surface motor of the motors to actuate the control surface to impact an orientation of the aircraft and operate a windshield wiper motor of the motors to actuate the windshield wipers.

Abstract: A secondary power distribution box (SPDB), solid state power controller (SSPC) line replacement module or printed board assembly (LRM/PBA), integrated power distribution and avionics system, and method of power distribution are disclosed. For example, the method includes receiving electrical power from a power source at a power feeder network, communicating with at least one load of a plurality of loads at least in part over the power feeder network, and coupling the electrical power to the at least one load of the plurality of loads in response to the communicating.

Abstract: A secondary power distribution box (SPDB), solid state power controller (SSPC) line replacement module or printed board assembly (LRM/PBA), integrated power distribution and avionics system, and method of power distribution are disclosed. For example, the method includes receiving electrical power from a power source at a power feeder network, communicating with at least one load of a plurality of loads at least in part over the power feeder network, and coupling the electrical power to the at least one load of the plurality of loads in response to the communicating.

Abstract: An aircraft taxi path guidance and display system is provided. The aircraft taxi path guidance and display system includes or cooperates with at least one source of aircraft status data, and a source of airport feature data associated with an airport field. The aircraft taxi path guidance and display system includes a processor operationally coupled to the source of aircraft status data and to the source of airport feature data. In response to aircraft status data and airport feature data, the processor predicts undesired deviations from an active surface area (e.g., an excursion). The processor generates corrective action associated with the excursion, and displays symbology that is graphically representative of the corrective action.

Abstract: An aircraft taxi path guidance and display system is provided. The aircraft taxi path guidance and display system includes or cooperates with at least one source of aircraft status data, and a source of airport feature data associated with an airport field. The aircraft taxi path guidance and display system includes a processor operationally coupled to the source of aircraft status data and to the source of airport feature data. In response to aircraft status data and airport feature data, the processor predicts undesired deviations from an active surface area (e.g., an excursion). The processor generates corrective action associated with the excursion, and displays symbology that is graphically representative of the corrective action.