FIELD: physics.
SUBSTANCE: stereoscopic indicator system displaying three-dimensional information through the windshield of the aircraft contains information sensors, an on-board computer, a display with alternate playback images of two-dimensional projections of the three-dimensional information virtual space, a light-combining unit for combining images of the real out-cabin environment with images of two-dimensional projections of the three-dimensional information virtual space, received from the information sensors. The system also contains an active binocular filter comprising an aperture that is uniform for both binocular viewing zones with two mutually adjacent areas of alternate binary changing the optical transmission, the common boundary between which corresponds to the boundary between the two zones of the binocular viewing.
EFFECT: obtaining stereoscopic images of the out-cabin environment.
4 cl, 2 dwg
