000			00665 a2200241 4500
001			274324
020			_a
041			_aeng
080			_aLNASA TM 4099 : 1989
245			_aEstimation of longitudinal stability and control derivatives for an Icing research aircraft from flight data
250			_a
260			_aWashington, D.C.
260			_bNational Aeronautics and Space Administration(NASA)
260			_c1989
300			_a22 p.
300			_c
856			_u
490			_aNASA TM 4099 : 1989
700			_a
650			_a
650			_aIcing, System identification, Stepwise regression, Cramer-Rao bounds, Aircraft stability and control
942			_cPP
942			_2UDC
999			_c230984 _d230984