Patent application number | Description | Published |
20080252636 | Synthesis Method for Intervisibility Images - The field of the invention is that of synthesis methods for a map image which is composed of pixels and represents the distribution of the intervisibility regions on a terrain overflown by an aircraft. The image synthesis method according to the invention provides both a two-dimensional cartographic representation in plan view of a terrain (T) overflown by an aircraft. The terrain has at least one potential threat (M), the intervisibility region, set of locations from where the aircraft is likely to be visible to said threat, being represented by at least one plain color. A second representation represents a view in vertical cross section of the terrain overflown. The second representation has a cross-sectional view of the intervisibility region. Various configurations of the first and of the second representations are proposed. | 10-16-2008 |
20100194601 | Device for Presenting and Selecting Data on a Display Screen - The general field of the invention is that of display devices for the management of systems comprising at least means of generating and displaying information concerning the system and a designator. The devices according to the invention are such that: | 08-05-2010 |
20100201546 | Device for the Temporary Presentation of Data on a Viewing Screen - The general field of the invention is that of the viewing devices used for the management of complex systems. The viewing device comprises the following functionalities:
| 08-12-2010 |
20110001698 | Visualization Device Comprising at Least One Prohibited Zone and a Pointer - The visualization device comprising computation means, display means including at least one prohibited zone and a system for guiding a pointer is characterized in that the pointer can remain immobile in the prohibited zone only for a limited duration, the pointer being automatically directed toward the outside of the prohibited zone after this limited duration. | 01-06-2011 |
20110046868 | Aircraft Guidance System for Assisting in Airport Navigation - An aircraft guidance system for assisting in airport navigation includes: at least one airport database comprising topology data of an airport, called airport DB; at least one configuration database comprising aircraft configuration data and the position of a guidance point; a positioning system delivering aircraft kinematic and attitude parameters; at least one computer generating a 2D view of the representation of the airport notably comprising navigation indications and a representation of the aircraft; and at least one display for displaying the representation of the airport. In the system, a first symbol is generated on the display indicating the position of an early guidance point, corresponding to the position of the guidance point at a future time. | 02-24-2011 |
20130215242 | METHOD FOR DISPLAYING INFORMATION IN A STEREOSCOPIC OR BINOCULAR DISPLAY SYSTEM - The general field of the invention is that of the methods for displaying at least two non-stereoscopic images of a different nature intended to be superposed so as to form only one final image. The method according to the invention comprises the following two successive steps:
| 08-22-2013 |
20130231804 | DEVICE FOR DISPLAY AND CONTROL OF SETPOINTS FOR AUTOMATIC PILOTING FOR AIRCRAFT - The general field of the invention is that of devices for display and control of setpoints for automatic piloting for aircraft, configured to display the setpoints of speed, heading, climb slope and altitude. The various setpoints are displayed in the form of a graphical representation comprising: wheels graduated in speed and in altitude indicating the aircraft setpoint values; a circular heading rose, graduated and centred on a first symbol representing the aircraft, the heading setpoint being indicated by a second symbol representing the heading to be followed by the aircraft and disposed around the perimeter of the heading rose; and a vertical sectional view comprising a graduated semicircle centred on a third symbol representing the aircraft, the slope setpoint being indicated by a fourth symbol representing the slope to be followed by the aircraft and disposed around the perimeter of the semicircle. | 09-05-2013 |
20140055323 | VISUALISATION SYSTEM, NOTABLY FOR AN AIRCRAFT, WITH A TRANSPARENT SCREEN AND WITH PERIPHERAL SYMBOLOGY - The general field of the invention is that of visualisation systems for an aircraft comprising a semi-transparent screen and electronic means suitable for generating a symbology displayed on said semi-transparent display screen, the symbology representing a parameter necessary for the piloting or navigation of the aircraft. The symbology according to the invention is partially or totally located on the periphery of the screen and comprises at least one moving pattern or a plurality of moving patterns, the speed and direction of the movement representing the relative difference between the value of the parameter at the present time and a reference value of said parameter, the patterns being immobilised when the value of the parameter at the present time attains said reference value. Different representations and different movements of the patterns are possible. | 02-27-2014 |
20150073696 | METHOD FOR SYNTHETIC THREE-DIMENSIONAL CONFORMAL REPRESENTATION OF TERRAIN CARTOGRAPHY AS A FUNCTION OF VISIBILITY - The general field of the invention is that of methods for three-dimensional conformal representation of a terrain. The method is used in a piloting and navigation assistance system of an aircraft. The assistance system comprises a navigation system, a cartographic database, electronic calculation means (CE) a meteorological database and a display system allowing the superimposition of synthetic images on the exterior. The method comprises the following steps: Step 1: Calculation, for a determined position of the vehicle, of the terrain perceptible through the display system; Step 2: Selection of a part of the said terrain as a function of a distance or of an altitude or of a range of altitudes; Step 3: Calculation of a three-dimensional conformal cartographic representation of the said selected part of the terrain; and Step 4: Display of the said cartographic representation by the display system. | 03-12-2015 |