Determining aircraft dynamics and position using gps...

G - Physics – 01 – C

Patent

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G01C 23/00 (2006.01) G01S 5/14 (2006.01)

Patent

CA 2379702

The present invention is a method and apparatus to determine flight parameters of an aircraft. Data received from a global positioning system (GPS) receiver are converted to position data. The position data are filtered based on a least-squares fitting to generate smoothed position data which provide the flight parameters.

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