Abstract:
Aviation is rapidly growing, particularly in developing countries, and there is a great need for understanding the mathematical modeling required in the training with more sophisticated aircraft in increasingly crowded and complex airspace. This paper modeled (y = 0.010x - 0.04 at R2= 0.9920) the aircraft pressure altimeters as a singular parameter with the elevation of the aircraft above a defined datum of 10, 20, 30, 40, 50, 60, 70, 80, 90 and 100 feet at a constant and standard QNH of 1,013.3 hectopascal which is practically the pressure on the altimeter's subscale above the sea level to establish a linear relationship with the indicated altitudes at the same unit status.
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