Abstract: A method of inspecting an air data probe for damage or misalignment on a mounting surface includes retrieving reference data for the air data probe from a database, capturing images of the air data probe via a camera and generating dimensions from the captured images of the air data probe via a feature extractor. An alignment calculator analyzes the generated dimensions from the captured images of the air data probe and the reference data for the air data probe from the database to identify misalignment of the air data probe, and analyzes the generated dimensions from the captured images of the air data probe and the reference data for the air data probe from the database to identify damage of the air data probe. A maintenance recommendation for the air data probe is generated and outputted, based on the identified misalignment or damage of the air data probe.

Abstract: A Wireless Avionics Intra-Communication (WAIC) system includes a communication network and a WAIC adapter location system. The communication network is configured to exchange data with a portable wireless device via WAIC adapter. The WAIC adapter location system is configured to determine a location of the WAIC adapter, which selectively connects and disconnects the portable device from the communication network based on the location.

Abstract: A locking system for an overhead stowage bin may comprise a latch and an electromechanical actuator configured to actuate the latch. A bin controller may be electrically coupled to the electromechanical actuator. A passenger input and a master controller may be in operable communication with the bin controller.

Abstract: Provided are embodiments for a method for monitoring a wiper system, the method includes reading a radio frequency identification (RFID) tag embedded in a wiper blade using a reader, comparing the read RFID tag to stored wiper blade information, determining a blade usage ratio for the wiper blade based on determining whether the wiper blade has been replaced, and providing an indication of a status of the wiper blade based at least in part on the blade usage ratio. Also provided are embodiments for a system for monitoring the health of the wiper system.

Abstract: A windscreen wiper system (WWS) architecture is provided. The WWS architecture includes a wiper assembly and an electronic control unit (ECU) configured to control operations of the wiper assembly. The ECU is configured to recognize that a command to engage a predefined wiper mode is received. The predefined wiper mode is characterized in that a windscreen is divided into sectors and the wiper assembly is controllably operated to sweep across one or more of the sectors in a predefined pattern with a predefined sweep speed. The ECU is further configured to control the wiper assembly to operate in the predefined wiper mode according to the command being received.

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 include techniques for a method and system for an augmented reality-based aircraft cargo monitoring and control system. The embodiments include a controlling device in communication with a master control panel (MCP), wherein the controlling device include a capturing module that is configured to receive an image and an object identification module that is configured to detect an identifier of an object from the image. The controlling device also includes a tracking module that is configured to track movement of the object, a rendering module that is configured to overlay an indicator over the image, and a microprojector that is configured to project the image on a display, wherein the display configured to display the mode and status of the object.

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: Disclosed is a method of operating a Portable Cargo Panel (PCP) for an aircraft, including: detecting a gesture on a display of the PCP; determining that the gesture is a command to view on the display a first cargo compartment; securing a wireless connection with the first control panel therein; receiving, from the first control panel, a health state of each of a plurality of Cargo Handling Units (CHUs) therein; displaying, on the display, the first cargo compartment with the plurality of CHUs and the operational state of the plurality of CHUs; controlling one or more of the CHUs in the first cargo compartment by transmitting, to the first control panel, a command to: run a diagnostic test against the one or more of the plurality of CHUs; or control the plurality of CHUs to move a Unit Load Device (ULD) into, within or out of the first cargo compartment.

Abstract: An article of manufacture may include a tangible, non-transitory computer-readable storage medium having instructions stored thereon for orienting a display of a portable electronic device configured to control a cargo handling system. The instructions, in response to execution by a processor, cause the processor to perform operations which may comprise identifying an optical label scanned by a camera of the portable electronic device, determining a viewing angle of the camera relative to the optical label, and determining an orientation of the display of the portable electronic device based on the viewing angle of the camera relative to the optical label.

Abstract: An article of manufacture may include a tangible, non-transitory computer-readable storage medium having instructions stored thereon for orienting a display of a portable electronic device configured to control a cargo handling system. The instructions, in response to execution by a processor, cause the processor to perform operations which may comprise identifying an optical label scanned by a camera of the portable electronic device, determining a viewing angle of the camera relative to the optical label, and determining an orientation of the display of the portable electronic device based on the viewing angle of the camera relative to the optical label.

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 Wireless Avionics Intra-Communications (WAIC) interface device provides communication between a portable electronic device and a WAIC controller. The WAIC interface device includes a housing, a wireless antenna, wireless access point electronics, and an interface controller. The housing is configured to be mounted to an interior surface of an aircraft and to receive and engage the portable electronic device. The wireless access point electronics are connected via a communication port to a first wired connection to communicate with the WAIC controller. The interface controller authenticates the portable electronic device. A WAIC coordinator is connected to the WAIC controller via a second wired connection, and is configured to communicate wirelessly over a WAIC frequency range between 4.2 gigahertz (GHz) and 4.4 GHz. An end node includes a transceiver configured to communicate wirelessly with the WAIC coordinator over the WAIC frequency range between 4.2 gigahertz (GHz) and 4.4 GHz.

Abstract: A Wireless Avionics Intra-Communication (WAIC) system includes a communication network and a WAIC adapter location system. The communication network is configured to exchange data with a portable wireless device via WAIC adapter. The WAIC adapter location system is configured to determine a location of the WAIC adapter, which selectively connects and disconnects the portable device from the communication network based on the location.

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: A windshield wiper system (WWS) is provided. The WWS includes a brushless direct current (BLDC) motor, a wiper arm and blade, a gearbox/converter operably interposed between the BLDC motor and the wiper arm and blade and a smart motor drive configured to determine a WWS failure condition and to operate the BLDC motor according to the determination.

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 include techniques for a method and system for an augmented reality-based aircraft cargo monitoring and control system. The embodiments include a controlling device in communication with a master control panel (MCP), wherein the controlling device include a capturing module that is configured to receive an image and an object identification module that is configured to detect an identifier of an object from the image. The controlling device also includes a tracking module that is configured to track movement of the object, a rendering module that is configured to overlay an indicator over the image, and a microprojector that is configured to project the image on a display, wherein the display configured to display the mode and status of the object.

Abstract: A Wireless Avionics Intra-Communications (WAIC) interface device provides communication between a portable electronic device and a WAIC controller. The WAIC interface device includes a housing, a wireless antenna, wireless access point electronics, and an interface controller. The housing is configured to be mounted to an interior surface of an aircraft and to receive and engage the portable electronic device. The wireless access point electronics are connected via a communication port to a first wired connection to communicate with the WAIC controller. The interface controller authenticates the portable electronic device. A WAIC coordinator is connected to the WAIC controller via a second wired connection, and is configured to communicate wirelessly over a WAIC frequency range between 4.2 gigahertz (GHz) and 4.4 GHz. An end node includes a transceiver configured to communicate wirelessly with the WAIC coordinator over the WAIC frequency range between 4.2 gigahertz (GHz) and 4.4 GHz.