The field of the invention is that of headset viewing systems, used in particular in the aeronautical field.
Headset viewing systems have commonly been used for aeronautical applications for several decades. A headset viewing system mainly comprises two sub-assemblies. The first is a headset equipped with a viewing system projecting toward the user's eye or eyes a collimated image superimposed on the exterior. The second is a headset posture detection system making it possible to reference in space, with respect to a known frame of reference, generally tied to an aircraft, the position and the orientation of the headset.
The main function of the headset viewing system is to be able to present, superimposed on the exterior landscape, so-called “conformal” information, that is to say displayed virtually in the exact direction that it would occupy in the exterior landscape. Thus, if the system displays a video image arising from a sensor and comprising a certain number of objects, the objects represented of this image are exactly superimposed on the real objects present on the terrain. By way of example,
However, the pilot may be led to consult documentation relating either to his aircraft, or to the flight, or to the mission in progress. This documentation exists either in the form of paper documentation, or, for a few years, has existed in electronic form. This type of electronic equipment is known by the name “EFB”, the acronym standing for “Electronic Flight Bag”. The documentation can also be displayed on the main viewing screens situated on the instrument panel of the cockpit. In all cases, the user must necessarily accommodate in order to pass from external vision to the reading of his documentation which is in paper form or in digital form. Moreover, the information provided by the viewing system is lost. Finally, consultation of paper documentation requires him to release the controls for a few moments.
The object of the invention is to implement novel means making it possible to display and to manage aeronautical documentation through the headset viewing system. In-flight consultation of this documentation is thus significantly simplified, without appreciably modifying the headset viewing system. More precisely, the subject of the invention is a headset viewing system 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, characterized in that the viewing system comprises a documentary data base and means for displaying and managing said documentary data as a function of the posture of the headset.
Advantageously, the appearance and the display of said data in the viewing device is conditioned by an orientation of the headset in a determined orientation range.
Advantageously, once they have appeared, the location of the data displayed in the viewing device is fixed in the known reference frame and independent of slight changes of posture of the headset not exceeding a few degrees.
Advantageously, once they have appeared, the data being structured in the form of pages, an entire page being presented in the viewing device, the rightward or leftward changing of pages is performed by modifying the posture of the headset leftward or rightward by at least several degrees.
Advantageously, the display of the data in the viewing device is located at the center and in the top part of the viewing device.
The invention will be better understood and other advantages will become apparent on reading the nonlimiting description which follows and by virtue of the appended figures among which:
A headset viewing system according to the invention mainly comprises:
The first function of the electronic computer is to ensure the generation of a conformal symbology superimposed on the exterior landscape by the optoelectronic display assembly. This symbology generally comprises the basic information necessary for piloting such as the indications of the speed, of the altitude, of the attitude, of the horizon, etc. To ensure this function, the various sensors of the aircraft provide the computer with the necessary information. The headset orientation detection system gives it the position and orientation information making it possible to display the symbology in a conformal manner, that is to say in a terrestrial frame of reference independent of the movements of the aircraft and of the movements of the headset.
The second function of the computer, and which is more particularly dedicated to the implementation of the invention, is the management of the display of the data of the documentary base as a function of the posture of the headset.
None of these electronic functions poses any particular difficulties for the person skilled in the art.
By way of example,
Preferentially, the documentation is tied to the aircraft frame of reference and therefore does not shift in case of slight head movements not exceeding a few degrees.
Preferentially, the documentation is organized in the form of sheets P referenced and/or numbered as seen in
The documentation may be consulted in the following manner. The rightward or leftward changing of pages is performed by modifying the posture of the headset leftward or rightward by at least several degrees. This change of page is illustrated in
Number | Date | Country | Kind |
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1400506 | Feb 2014 | FR | national |
Filing Document | Filing Date | Country | Kind |
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PCT/EP2015/053147 | 2/13/2015 | WO | 00 |