Abstract: A vehicle management system (VMS) computer includes a processor and a memory coupled to the processor by a bus. The VMS computer also includes a power distribution controller that includes a plurality of power distribution circuits that are each controlled by the controller to supply power to a plurality of end component loads. The power distribution controller is communicably coupled to the processor and the memory by the bus. The VMS computer also includes a plurality of parallel power distribution lines. Each pair of parallel power distribution lines couples a respective one of the plurality of power distribution circuits to a corresponding one of a plurality of end component loads. Each of the plurality of power distribution circuits supplies power via both lines in a respective pair of the plurality of parallel power distribution lines.

Abstract: An avionics mounting unit includes a housing with a first mounting interface to couple the housing to a structure of an aircraft and a second mounting interface to couple an avionics device to the housing. The second mounting interface includes slots oriented orthogonal to each other and extending to sides of the housing such that the avionics device can be installed via the slots from any of four sides of the housing. The avionics mounting unit also includes communication circuitry, power supply circuitry, one or more avionics device interface ports, and one or more aircraft interface ports. The avionics device interface port(s) are configured to provide power to the avionics device and configured to enable data communications with the avionics device. The aircraft interface port(s) are configured to receive power from the aircraft and to enable data communications between other aircraft systems and the avionics device.

Abstract: A vehicle management system (VMS) computer includes a data processing system comprising a processor, a memory, and a power distribution controller. The power distributions controller includes a plurality of power distribution circuits that are each controlled by the controller to supply power to end component loads. The power distribution controller is communicably coupled to the data processing system by a bus. The power distribution controller is configured to control power generation by each of the plurality of power distribution circuits such that each of the plurality of power distribution circuits generates output power at an adjustable voltage level output to a respective one of the end component loads.

Abstract: A vehicle management system (VMS) computer includes a processor and a memory coupled to the processor by a bus. The VMS computer also includes a power distribution controller that includes a plurality of power distribution circuits that are each controlled by the controller to supply power to a plurality of end component loads. The power distribution controller is communicably coupled to the processor and the memory by the bus. The VMS computer also includes a plurality of parallel power distribution lines. Each pair of parallel power distribution lines couples a respective one of the plurality of power distribution circuits to a corresponding one of a plurality of end component loads. Each of the plurality of power distribution circuits supplies power via both lines in a respective pair of the plurality of parallel power distribution lines.

Abstract: A vehicle management system (VMS) computer includes a data processing system comprising a processor, a memory, and a power distribution controller. The power distributions controller includes a plurality of power distribution circuits that are each controlled by the controller to supply power to end component loads. The power distribution controller is communicably coupled to the data processing system by a bus. The power distribution controller is configured to control power generation by each of the plurality of power distribution circuits such that each of the plurality of power distribution circuits generates output power at an adjustable voltage level output to a respective one of the end component loads.

Abstract: A vehicle management system (VMS) computer includes a power distribution controller that includes a plurality of power distribution circuits that are each controlled by the controller to supply power to end component loads. The power distribution controller is communicably coupled to a data processing system by a bus. The VMS computer also includes a plurality of settable circuit breakers, wherein each of the plurality of settable circuit breakers corresponds to a respective one of the plurality of power distribution circuits. The power distribution controller is configured to monitor various values such as voltages, currents, powers, power spikes, and interruptions and to interrupt a respective one of the plurality of power distribution circuits via a settable circuit breaker upon detecting an indication of a fault from the monitored values.

Abstract: An avionics mounting unit includes a housing with a first mounting interface to couple the housing to a structure of an aircraft and a second mounting interface to couple an avionics device to the housing. The second mounting interface includes slots oriented orthogonal to each other and extending to sides of the housing such that the avionics device can be installed via the slots from any of four sides of the housing. The avionics mounting unit also includes communication circuitry, power supply circuitry, one or more avionics device interface ports, and one or more aircraft interface ports. The avionics device interface port(s) are configured to provide power to the avionics device and configured to enable data communications with the avionics device. The aircraft interface port(s) are configured to receive power from the aircraft and to enable data communications between other aircraft systems and the avionics device.