An extended Kalman filter (EKF) algorithm is implemented on UNIVAC 1100/70. As an example, the longitudinal states, characterizing the short period dynamics of an aircraft are obtained from noisy measured data. This algorithm, with minor modifications and the incorporation of a stiff differential equation solution algorithm, could be implemented for extraction of stability and control derivatives from noisy flight test data.
Extended Kalman Filter (EKF) Algorithm
1989
13 pages
Report
Keine Angabe
Englisch
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