Patent classifications
G09B9/323
SYSTEM AND METHOD OF ADJUSTING FOCAL DISTANCES OF IMAGES DISPLAYED TO A USER OF A SIMULATOR
Systems and methods for adjusting focal distances of images displayed to a user at a designated eye point of a simulator are provided. An image may be generated for display by a screen, wherein the image is reflected by a mirror to the designated eye point. A simulated distance from the designated eye point to an object in the image may be determined. A focal distance for the image may be determined based on the simulated distance. A simulated size of the object may be determined based on the simulated distance. An adjustor may alter a distance between the screen and the mirror to achieve the focal distance. A size of the object may be adjusted in the image based on the simulated size.
System and method for adjusting the correlation between a perspective of an onboard visual display and a current orientation of an inflight aircraft
Methods are provided for adjusting any correlation between a perspective of an onboard visual display and a current orientation of an inflight aircraft. The method comprises determining the current orientation of the inflight aircraft and determining the perspective of the visual display. The visual display is shown to a pilot of the inflight aircraft on a display element located onboard the inflight aircraft. The current orientation of the aircraft is compared with the perspective of the visual display to determine if the perspective of the visual display needs to transition to reflect the current orientation of the aircraft. If the display does need to be changed, a rate of transition of the visual display's perspective is selected based on current aircraft performance parameters. The perspective of the visual display is then transitioned to reflect the current orientation of the aircraft at the selected rate.
SYSTEM AND METHOD FOR ADJUSTING THE CORRELATION BETWEEN A PERSPECTIVE OF AN ONBOARD VISUAL DISPLAY AND A CURRENT ORIENTATION OF AN INFLIGHT AIRCRAFT
Methods are provided for adjusting any correlation between a perspective of an onboard visual display and a current orientation of an inflight aircraft. The method comprises determining the current orientation of the inflight aircraft and determining the perspective of the visual display. The visual display is shown to a pilot of the inflight aircraft on a display element located onboard the inflight aircraft. The current orientation of the aircraft is compared with the perspective of the visual display to determine if the perspective of the visual display needs to transition to reflect the current orientation of the aircraft. If the display does need to be changed, a rate of transition of the visual display's perspective is selected based on current aircraft performance parameters. The perspective of the visual display is then transitioned to reflect the current orientation of the aircraft at the selected rate.
System and method for adjusting the correlation between a visual display perspective and a flight path of an aircraft
Methods are provided for adjusting any correlation between a visual display perspective and a default display view of an aircraft. The method comprises determining the default display view for an inflight aircraft and determining the orientation of the visual display for the crew of the aircraft. The default display view is compared with the orientation of the visual display to determine if the visual display's perspective needs to be transitioned to reflect the default display view. If the display does need to be changed, the rate of transition of the visual display's perspective is selected based on current aircraft performance parameters.
SYSTEM AND METHOD FOR ADJUSTING THE CORRELATION BETWEEN A VISUAL DISPLAY PERSPECTIVE AND A FLIGHT PATH OF AN AIRCRAFT
Methods are provided for adjusting any correlation between a visual display perspective and a default display view of an aircraft. The method comprises determining the default display view for an inflight aircraft and determining the orientation of the visual display for the crew of the aircraft. The default display view is compared with the orientation of the visual display to determine if the visual display's perspective needs to be transitioned to reflect the default display view. If the display does need to be changed, the rate of transition of the visual display's perspective is selected based on current aircraft performance parameters.