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                - inverselerp(0,"THRUST", -1 * ("MASS" * ((-1 * TAS * TAS ) / (2 * (AltitudeAgl - "HOVERZONE")) - 9.8))) * clamp01(AltitudeAgl > "HOVERZONE" + "BUFFER") * clamp01(AltitudeAgl < "BURN START" )
 - Local CONSTANTS:
 - -THRUST: The maximum thrust of your engine. (Newtons)
 - -MASS: Mass of the craft. (KG)
 - -HOVERZONE: The equation will have the device perfectly stop at this point. (Meters)
 - -BUFFER: The system will cut out the engine landing sequence at this altitude, above the HOVERZONE. That way it lands and doesn't hover at 0m/s. (Meters above HOVERZONE, recc. 0.1)
 - -BURN START: The altitude AGL the craft will start its landing burn (The lower, the more thrust required to land safely)
 
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