On-line estimation and identification of aircraft stability derivatives using the modified gain extended Kalman filter
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[1] J. Speyer,et al. A stochastic analysis of a modified gain extended Kalman filter with applications to estimation with bearings only measurements , 1983 .
[2] Arthur E. Bryson,et al. Wind Modeling and Lateral Control for Automatic Landing (Originally schedulled for publication in the Journal of Aircraft) , 1977 .
[3] Jason L. Speyer,et al. Multi-input/multi-output controller design for longitudinal decoupled aircraft motion , 1984 .
[4] Jason L. Speyer,et al. The Modified Gain Extended Kalman Filter and Parameter Identification in Linear Systems , 1984, 1984 American Control Conference.