Estimation of longitudinal stability and control derivatives for an Icing research aircraft from flight data

Estimation of longitudinal stability and control derivatives for an Icing research aircraft from flight data - - Washington, D.C. National Aeronautics and Space Administration(NASA) 1989 - 22 p. - NASA TM 4099 : 1989 .





Icing, System identification, Stepwise regression, Cramer-Rao bounds, Aircraft stability and control

LNASA TM 4099 : 1989

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