In an aspect of the present disclosure is a system for monitoring health of a motor, including at least one sensor configured to detect at least a motor metric and send motor datum based on the at least a motor metric, an augmented reality display configured to display a visual representation of the motor datum, and a computing device communicatively connected to the at least one sensor and the augmented reality display, wherein the computing device is configured to: receive the motor datum from the at least one sensor; and command the augmented reality display to display the visual representation of the motor datum.

Augmented reality display systems, apparatuses, and methods are disclosed for enabling a wearer of an augmented reality optical display to continue wearing the same optical display while moving between different platforms or vehicles. Example embodiments include optical displays that use a wired connection to connect with each platform to minimize the electromagnetic signature of the system. Embodiments include changing the information displayed to the user depending on the type of vehicle to which the optical display is connected. Additional embodiment display information about weapon systems associated with the platform to which the optical display is connected.

A sidewall assembly for an aircraft and an aircraft are provided. In one example, the sidewall assembly includes a window. A sidewall portion has an inner-facing side and at least partially surrounds the window. The sidewall portion and the window have a curved contour. A transparent display panel is coupled to the sidewall portion and covers the inner-facing side of the sidewall portion including the window. The transparent display panel includes a display screen configured to display information to a passenger. The transparent display panel including the display screen have a curved contour that substantially matches the curved contour of the sidewall portion and the window. A display controller is in communication with the transparent display panel to communicate a video/audio signal providing the information to the display screen.

The invention relates to this method comprising the following steps, for at least one input/output parameter: duplicating and inserting a list of graphical commands associated with said parameter within a calculation module of said chain, from a current value of said parameter, obtaining a current cyclic redundancy code associated with a current micropattern, generated by executing said at least one list, comparing said current cyclic redundancy code with a reference cyclic redundancy code stored in a dedicated memory space for a substantially identical value of said parameter within a tolerance threshold, in the event of a difference in cyclic redundancy code value, automatic sanctioning of said chain at least by suspending its execution.

A smart landing pad comprises a flexible display that shows images or patterns, and a protective layer over the display. The protective layer allows a UAV to land without damaging the display. Locator and range finder devices, coupled to the display, communicate with the UAV. The display is operative for wireless communications with a computer or mobile device that provides on-demand user functions, allowing for dynamically changing or customizing the images/patterns shown on the display. The images/patterns comprise a background area showing changeable images that match an environment where the landing pad is placed, and a target landing area surrounded by the background area. The target landing area includes a changeable insensitive, contrast portion, and changeable marker pattern portions having changeable colors/shapes. The images/patterns also include changeable QR codes on the target landing area. The display is IoT enabled so that data from the landing pad is remotely cloud accessible.

The invention concerns an automatic flight controller with operating elements, by means of which target settings of the automatic flight controller can be set by an operator, and with display elements for data display, wherein the display elements comprise at least two mutually separate displays that are disposed on the front, for example a front panel, of the automatic flight controller, wherein a) the at least two mutually separate displays are high resolution graphical displays and/or b) the automatic flight controller is designed to display all operating mode awareness-relevant parameters of the automatic flight controller on one or more of the at least two mutually separate displays of the automatic flight controller.

The invention further concerns an aircraft cockpit with such an automatic flight controller as well as a method for operating a flight controller. The invention also concerns a computer program for carrying out the method

A method and apparatus for inspecting an aircraft. The method displays, by a processor unit in a mobile device, a two-dimensional layout of an interior of an aircraft on a graphical user interface on the mobile device in which the two-dimensional layout includes fixed features visible within the interior of the aircraft. The method displays, by the processor unit, a three-dimensional view of a group of objects in the aircraft on the graphical user interface on the mobile device with a point-of-view at a selected distance from an object in the group of objects and in a direction when a fixed feature corresponding to the object is selected from the fixed features in the two-dimensional layout using an input system for the mobile device. The method changes, by the processor unit, the direction of the three-dimensional view in response to movement of the mobile device.

A system method for providing aircraft lateral navigation system capability feedback to a pilot includes determining, in a processor, when a flight plan has been received that includes a flight leg that needs to be captured by the aircraft. A determination is made, in the processor, when an armed signal has been received, where the armed signal indicating that an aircraft autopilot navigation mode (NAV) has been armed. The processor is used to command a display device to render the flight leg using a first display paradigm when the armed signal has not been received, and to render the flight leg using a second display paradigm when the armed signal has been received.

A method is present for presenting a flight deck. A model of the flight deck is identified having a number of locations for a number of displays. Aircraft data is obtained. A number of panels is generated from the aircraft data. A display of the flight deck is generated containing the number of panels in the number of locations to form a presentation of the flight deck.

Systems and methods of displaying data are provided. A display system can include one or more display windows configured to provide for display graphical representations of data. One or more user applications can be configured to provide data to the display system. The display system is configured to receive data indicative of a user request to view display data, provide for display on at least one of the one or more display windows a first subset of the display data, obtain one or more data sets corresponding to a second subset of the display data from at least one of the one or more user applications, subsequent to obtaining the one or more data sets, and provide for display on at least one of the one or more display windows the second subset of the display data.