Abstract: Provided is a selection unit for selecting different states or functions of an aircraft system, including: a manually operable selection element, the selection element including a first display indicating the actual selection state of the selection element, with each selection state of the selection element representing a different state or function of the aircraft system, wherein the selection element is additionally designed and configured for a dynamic electronic selection of the actual selection state based on an external signal input, and a second display co-located with the selection element, the second display visualizing the actual state of the aircraft system depending on the actual selection state of the selection element.

Abstract: An aircraft navigation system and a method for aircraft navigation is presented. The aircraft navigation system has a navigation-map data source, navigation-map data provided by the navigation-map data source including information about a multitude of objects O on earth surface which are of high potential visibility and high potential identifiability from elevated positions, each information for an object O?O including a position and a type of the respective object O; a first system for measuring an actual aircraft position P(t); a waypoint data source providing waypoints WPi defining an aircraft intended flight track; a second system for selecting per waypoint WPi one object Oi(WPi) with Oi(WPi)?O depending on given selection criteria; and a display for displaying an information I(Oi(WPi) referring the selected object Oi(WPi).

Abstract: An aircraft navigation system and a method for aircraft navigation is presented. The aircraft navigation system has a navigation-map data source, navigation-map data provided by the navigation-map data source including information about a multitude of objects O on earth surface which are of high potential visibility and high potential identifiability from elevated positions, each information for an object O ? O including a position and a type of the respective object O; a first system for measuring an actual aircraft position P(t); a waypoint data source providing waypoints WPi defining an aircraft intended flight track; a second system for selecting per waypoint WPi one object Oi(WPi) with Oi(WPi) ? O depending on given selection criteria; and a display for displaying an information I(Oi(WPi) referring the selected object Oi(WPi).

Abstract: A display assembly for displaying a parameter of an aircraft, comprising a parameter device and a non-transparent display device. The parameter device for gathering a parameter of the aircraft and/or of an equipment of the aircraft includes a sending unit for sending the parameter. The non-transparent display device is detachable, is configured to display the parameter, and comprises a receiving unit for receiving the parameter. The sending unit transmits the parameter directly to the receiving unit.

Abstract: A method and device to create a realistic and flexible test environment for the evaluation of augmented reality application and device. The test method and the test device for testing the function and/or use of a head worn see through augmented reality device by means of a virtual reality environment, comprises a head mounted device. The head mounted display includes a virtual reality head mounted display configured to display the virtual reality environment to the eyes of a user through the head worn see through augmented reality device, and an alignment device to align the head mounted display and the head worn see through augmented reality device.

Abstract: A display assembly for displaying a parameter of an aircraft, comprising a parameter device and a non-transparent display device. The parameter device for gathering a parameter of the aircraft and/or of an equipment of the aircraft includes a sending unit for sending the parameter. The non-transparent display device is detachable, is configured to display the parameter, and comprises a receiving unit for receiving the parameter. The sending unit transmits the parameter directly to the receiving unit.

Abstract: In order to be able to test man-machine interfaces (74) cost-effectively under as realistic conditions as possible at as early a stage as possible, a method for testing at least one device (56) to be operated in aircraft by means of a virtual reality environment, wherein the at least one device (56) to be tested is represented in a virtual manner to a test subject (20), and an interaction between the test subject (20) and the at least one device (56) is recorded by means of or in the virtual reality environment.

Abstract: Provided is a selection unit for selecting different states or functions of an aircraft system, comprising: a manually operable selection element, the selection element comprising a first display indicating the actual selection state of the selection element, with each selection state of the selection element representing a different state or function of the aircraft system, wherein said selection element is additionally designed and configured for a dynamic electronic selection of the actual selection state based on an external signal input, and a second display co-located with the selection element, the second display visualizing the actual state of the aircraft system depending on the actual selection state of the selection element.