Abstract:
The general field of the invention is that of headset viewing systems comprising at least one headset equipped with a viewing device and a system for detecting posture of said headset with respect to a known reference frame. The viewing system according to the invention comprises a documentary data base and means for displaying and managing said documentary data as a function of the posture of the headset.
Abstract:
The general area of the invention is that of methods for managing flight plans by an avionic system comprising a visualization device and a touch-sensitive interface. The visualization device displays a cartographic representation of the terrain flown over, aeronautical data and a flight plan composed of a set of segments connecting together certain aeronautical waypoints. The management method contains several steps, a first editing step activated by touch-sensitive designating of any point of the flight plan, a second modification of the flight plan step activated by a touch-sensitive movement, the end of the touch-sensitive movement triggering a movement or an addition or the removal of a waypoint. The method also makes it possible to easily manage the airways in order to incorporate them into a flight plan during modification.
Abstract:
The general field of the invention is that of avionics systems intended to be used on aircraft in flight above a terrain. The avionics system comprises a display system and a navigation system. The display system comprises a head support equipped with a display device capable of generating images overlaid on said terrain, and a system for detecting posture of said helmet. The display system according to the invention comprises means for displaying a marking symbol in the display device, said symbol determining a given direction. The navigation system comprises geolocation means for said aircraft, a database of cartographic data representative of said terrain and computation means making it possible to determine the location of the area of the terrain arranged at the intersection of said given direction with said terrain, and means for recording and processing said location in the navigation system.
Abstract:
The general field of the invention is that of head viewing systems for aircraft comprising a head support, a viewing device, a detection of posture of said head support, means for detecting the current heading of an aircraft and means for graphically generating said heading. The system according to the invention comprises means of control, display and selection of headings arranged so as: to display in response to a first command, a second so-called setpoint heading and a third heading termed a “support heading” corresponding to the direction of the head support in a terrestrial reference frame, said direction given by the information arising from the detection of posture of said head support and the means for detecting the current heading; to replace, in response to a second command, said second heading by said third heading, said third heading thus becoming the new heading setpoint.
Abstract:
The general field of the invention is that of methods of graphical representation, modification and validation of an aeronautical flight plan for an aircraft avionics system. Said system comprises means for computing said flight plan, a system for managing the tasks necessary for the accomplishment of said flight plan, a visualization device displaying a graphical representation of said flight plan and a man-machine interface able to carry out selections, modifications or additions in the information contained in said graphical representation, said selections, modifications and additions being taken into account by the task management system. The graphical representation comprises a timeline on which feature at least the various phases of the flight plan and the corresponding information. The method comprises a step of displaying at least one first interactive graphical icon, representative of the overall state of progress of the tasks to be performed before a change of flight phase.