Method of inferring rotorcraft gross weight

Details Method of inferring rotorcraft gross weight Method of inferring rotorcraft gross weight

G - Physics

06

N

G06N 3/02 (2006.01) G01G 9/00 (2006.01) G01G 19/00 (2006.01) G01G 19/07 (2006.01) G06F 19/00 (2006.01)

Patent

CA 2457992

Described are systems and methods for determining the gross weight of an aircraft. A flight regime is determined based on one or more inputs. A neural net is selected based on a flight regime. The neural net inputs may include derived values. A first estimate of the gross weight is produced by the selected neural net. The first estimate is used, along with other inputs, with a Kalman filter to produce a final gross weight estimate. The Kalman filter blends or fuses together its inputs to produce the final gross weight estimate.

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