A method for rendering images on a display that is disposed within an aircraft, the method comprising the steps of: rendering an image, on the display, that includes one of, or both, rendered terrain and rendered sky, the rendered terrain and rendered sky representative of terrain and sky located outside of the aircraft, respectively, wherein the position and orientation of the rendered terrain and rendered sky is dependent upon the position and orientation of the aircraft; rendering a pitch tape on the display; rendering a zero pitch reference line on the display; and at least selectively or continuously rendering a sky veil on a portion of the display, the sky veil rendered at least partially transparent and in a manner that: (i) portions of the sky veil that overlap with rendered sky are not discernable, and (ii) rendered terrain is viewable through portions of the sky veil that overlap with terrain; (iii) the sky veil is perpendicular to the pitch tape and parallel to the zero pitch reference line; and (iv) the sky veil extends a predetermined distance (d) from a skyward edge as measured along a line that is parallel to the pitch tape, and wherein, during a roll condition of the aircraft when a roll angle is within a predetermined angular offset (θ), said offset being measured from an angle of a line between a center of an aircraft symbol shown on the display and an upper corner (604-1,604-2) of the display, such that the pitch tape approaches or is aligned with the upper corner (604-1, 604-2) of the display, instead continuously rendering the sky veil a predetermined distance (r) from a predetermined point, the predetermined point being the center of the aircraft symbol shown on the display, and along a tangent of a curve having a radius (r). rendering an image, on the display, that includes one of, or both, rendered terrain and rendered sky, the rendered terrain and rendered sky representative of terrain and sky located outside of the aircraft, respectively, wherein the position and orientation of the rendered terrain and rendered sky is dependent upon the position and orientation of the aircraft; rendering a pitch tape on the display; rendering a zero pitch reference line on the display; and at least selectively or continuously rendering a sky veil on a portion of the display, the sky veil rendered at least partially transparent and in a manner that: (i) portions of the sky veil that overlap with rendered sky are not discernable, and (ii) rendered terrain is viewable through portions of the sky veil that overlap with terrain; (iii) the sky veil is perpendicular to the pitch tape and parallel to the zero pitch reference line; and (iv) the sky veil extends a predetermined distance (d) from a skyward edge as measured along a line that is parallel to the pitch tape, and wherein, during a roll condition of the aircraft when a roll angle is within a predetermined angular offset (θ), said offset being measured from an angle of a line between a center of an aircraft symbol shown on the display and an upper corner (604-1,604-2) of the display, such that the pitch tape approaches or is aligned with the upper corner (604-1, 604-2) of the display, instead continuously rendering the sky veil a predetermined distance (r) from a predetermined point, the predetermined point being the center of the aircraft symbol shown on the display, and along a tangent of a curve having a radius (r). (i) portions of the sky veil that overlap with rendered sky are not discernable, and (ii) rendered terrain is viewable through portions of the sky veil that overlap with terrain; (iii) the sky veil is perpendicular to the pitch tape and parallel to the zero pitch reference line; and (iv) the sky veil extends a predetermined distance (d) from a skyward edge as measured along a line that is parallel to the pitch tape, and wherein, during a roll condition of the aircraft when a roll angle is within a predetermined angular offset (θ), said offset being measured from an angle of a line between a center of an aircraft symbol shown on the display and an upper corner (604-1,604-2) of the display, such that the pitch tape approaches or is aligned with the upper corner (604-1, 604-2) of the display, instead continuously rendering the sky veil a predetermined distance (r) from a predetermined point, the predetermined point being the center of the aircraft symbol shown on the display, and along a tangent of a curve having a radius (r).