| CPC B64D 45/08 (2013.01) [G08G 5/21 (2025.01); G08G 5/30 (2025.01); G08G 5/54 (2025.01)] | 20 Claims |

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1. A landing system for an aircraft, wherein:
the landing system is configured to calculate a reference path for use during a non-precision approach to a runway, the reference path comprising a course, a flight path angle, and an anchor point, the anchor point having a longitude, a latitude, and an altitude;
the landing system is configured to extract from a navigation database a missed approach point corresponding to a first landing threshold point of the runway, the missed approach point having a longitude, a latitude and an altitude;
the landing system is configured such that calculation of the reference path comprises setting the altitude of the anchor point with use of the altitude of the missed approach point;
the missed approach point is associated with the flight path angle;
the landing system is configured to extract from the navigation database a stored landing threshold point of the runway, the stored landing threshold point having a longitude, a latitude and an altitude; and
the landing system is configured such that calculation of the reference path comprises:
calculating a location of a pseudo final end point (pseudo-FEP) for the stored landing threshold point;
calculating a horizontal distance between the missed approach point and the pseudo-FEP so calculated; and
setting the altitude of the anchor point to a value equal to the altitude of the missed approach point less a vertical distance equal to the product of: (i) a tangent of the flight path angle associated with the missed approach point and (ii) the horizontal distance between the missed approach point and the pseudo-FEP so calculated.
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