Abstract: Provided are embodiments for a system having an avionics system that is configured to dynamically communicate one or more configurable parameters of a wiper and wash system based at least in part on a selected mode, and an avionics bus that is configured to communicate dynamic parameters from the avionics system. The system also includes a wash system having a fluid reservoir and fluid level sensor, and a wiper system including a control unit (ECU) that is configured to operate the system based at least in part on the one or more configurable parameters, wherein the wiper system is coupled to the wash system and supplies the wash fluid to the wiper system. Also provided are embodiments of a method for performing dynamic control of the aircraft windscreen wiper and wash system configuration parameters.

Abstract: Provided are embodiments for a system having an avionics system that is configured to dynamically communicate one or more configurable parameters of a wiper and wash system based at least in part on a selected mode, and an avionics bus that is configured to communicate dynamic parameters from the avionics system. The system also includes a wash system having a fluid reservoir and fluid level sensor, and a wiper system including a control unit (ECU) that is configured to operate the system based at least in part on the one or more configurable parameters, wherein the wiper system is coupled to the wash system and supplies the wash fluid to the wiper system. Also provided are embodiments of a method for performing dynamic control of the aircraft windscreen wiper and wash system configuration parameters.

Abstract: Provided are embodiments for a system having an avionics system that is configured to dynamically communicate one or more configurable parameters of a wiper and wash system based at least in part on a selected mode, and an avionics bus that is configured to communicate dynamic parameters from the avionics system. The system also includes a wash system having a fluid reservoir and fluid level sensor, and a wiper system including a control unit (ECU) that is configured to operate the system based at least in part on the one or more configurable parameters, wherein the wiper system is coupled to the wash system and supplies the wash fluid to the wiper system. Also provided are embodiments of a method for performing dynamic control of the aircraft windscreen wiper and wash system configuration parameters.

Abstract: Provided are embodiments that include techniques for a wireless portable cargo control panel with physical controls. The techniques include a portable electronic device (PED) including a display, the PED configured to communicate with a master control panel (MCP) that controls a cargo handling system and a portable control panel (PCP). The PCP includes an interface configured to couple the PED, one or more dedicated physical input selection devices, a directional controller, and one or more orientation indicator displays, wherein each of the one or more orientation indicator displays are configured to be updated based at least in part on orientation information associated with the cargo handling system, PCP, and PED.

Abstract: Embodiments include techniques for managing multiple portable control panels in aircraft cargo handling system are provided. The embodiments include a master control panel (MCP), and a plurality of wireless coordinators in communication with the MCP. The embodiments also include a plurality of zones of a cargo storage area, wherein each zone of the plurality of zones is defined by a portion of the cargo storage area that is controlled by a wireless coordinator of the plurality of wireless coordinators and includes at least one of power drive units (PDU) and turntables, and a plurality of portable control panels (PCP) in communication with the wireless coordinators, the PCP configured to operate and monitor states of the PDU and turntables.

Abstract: A system for monitoring and maintaining aircraft cargos includes a plurality of master control panels each operatively connected with at least one Line Replaceable Unit (LRU) operating in a cargo compartment of an aircraft, and at least one unit load device (ULD). The at least one ULD and at least one LRU are configured to move a cargo unit in the cargo compartment based on a control signal from the master control panel. The system also includes a command unit operatively connected with each control panel of the plurality of master control panels. The command unit includes a processor configured to retrieve a status of the cargo from each of the plurality of master control panels, and display, on an output device, a status of the at least one ULD of a plurality of ULDs and a status of the at least one LRU via the processor.

Abstract: Provided are embodiments for a system having an avionics system that is configured to dynamically communicate one or more configurable parameters of a wiper and wash system based at least in part on a selected mode, and an avionics bus that is configured to communicate dynamic parameters from the avionics system. The system also includes a wash system having a fluid reservoir and fluid level sensor, and a wiper system including a control unit (ECU) that is configured to operate the system based at least in part on the one or more configurable parameters, wherein the wiper system is coupled to the wash system and supplies the wash fluid to the wiper system. Also provided are embodiments of a method for performing dynamic control of the aircraft windscreen wiper and wash system configuration parameters.

Abstract: Embodiments includes a system and method for automatic orientation of a display for a portable electronic device (PED) of an aircraft cargo control and monitor panel. The system includes an attitude heading reference system for detecting a first heading information, a master control panel operably coupled to the attitude heading reference system, and a portable electronic device operably coupled to the master control panel. The PED includes a sensor for detecting a second heading information, a display, and a processor operably coupled to the sensor and the display. The processor is configured to receive the first heading information, receive the second heading information, where the first heading information is different than the second heading information, compare the first heading information and the second information, and modify an orientation of a presentation of the display based at least in part on the comparison.

Abstract: Provided are embodiments that include techniques for a wireless portable cargo control panel with physical controls. The techniques include a portable electronic device (PED) including a display, the PED configured to communicate with a master control panel (MCP) that controls a cargo handling system and a portable control panel (PCP). The PCP includes an interface configured to couple the PED, one or more dedicated physical input selection devices, a directional controller, and one or more orientation indicator displays, wherein each of the one or more orientation indicator displays are configured to be updated based at least in part on orientation information associated with the cargo handling system, PCP, and PED.

Abstract: Embodiments include techniques for managing multiple portable control panels in aircraft cargo handling system are provided. The embodiments include a master control panel (MCP), and a plurality of wireless coordinators in communication with the MCP. The embodiments also include a plurality of zones of a cargo storage area, wherein each zone of the plurality of zones is defined by a portion of the cargo storage area that is controlled by a wireless coordinator of the plurality of wireless coordinators and includes at least one of power drive units (PDU) and turntables, and a plurality of portable control panels (PCP) in communication with the wireless coordinators, the PCP configured to operate and monitor states of the PDU and turntables.

Abstract: Embodiments includes a system and method for automatic orientation of a display for a portable electronic device (PED) of an aircraft cargo control and monitor panel. The system includes an attitude heading reference system for detecting a first heading information, a master control panel operably coupled to the attitude heading reference system, and a portable electronic device operably coupled to the master control panel. The PED includes a sensor for detecting a second heading information, a display, and a processor operably coupled to the sensor and the display. The processor is configured to receive the first heading information, receive the second heading information, where the first heading information is different than the second heading information, compare the first heading information and the second information, and modify an orientation of a presentation of the display based at least in part on the comparison.

Abstract: A system for monitoring and maintaining aircraft cargos includes a plurality of master control panels each operatively connected with at least one Line Replaceable Unit (LRU) operating in a cargo compartment of an aircraft, and at least one unit load device (ULD). The at least one ULD and at least one LRU are configured to move a cargo unit in the cargo compartment based on a control signal from the master control panel. The system also includes a command unit operatively connected with each control panel of the plurality of master control panels. The command unit includes a processor configured to retrieve a status of the cargo from each of the plurality of master control panels, and display, on an output device, a status of the at least one ULD of a plurality of ULDs and a status of the at least one LRU via the processor.