| CPC G08G 5/34 (2025.01) [B64C 29/00 (2013.01); B64D 43/00 (2013.01); G08G 5/21 (2025.01)] | 20 Claims |

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1. A pilot display system for an aircraft, the system comprising:
a sensor configured to measure an aircraft position and generate a position datum based on the aircraft position;
a display incorporated in the aircraft; and
a computing device communicatively connected to the sensor and the display, the computing device configured to:
receive a flight path including a transition point;
determine, based at least in part on the position datum, the aircraft position relative to the transition point; and
command the display to display a visual representation of the aircraft position relative to the transition point, wherein the transition point represents a location along the flight path where the aircraft is transitioning between fixed-wing flight and vertical rotor-based flight or between vertical rotor-based and fixed-wing flight.
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