论文信息 - Missile aerodynamic identification using mixed EKF and EBM - 字舞流文

Missile aerodynamic identification using mixed EKF and EBM

Ali Mohammadi | Mohammad Massoumnia

[1] Ermin Plaetschke,et al. Identification of moderately nonlinear flight mechanics systems withadditive process and measurement noise , 1990 .

[2] R. V. Jategaonkar,et al. Evaluation of Parameter Estimation Methods for Unstable Aircraft , 1994 .

[3] Juan Garcia-Velo,et al. Aerodynamic Parameter Estimation for High-Performance Aircraft Using Extended Kalman Filtering , 1997 .

[4] Uri Shaked,et al. Robust minimum variance filtering , 1995, IEEE Trans. Signal Process..

[5] Harald Preissler,et al. Equation decoupling - A new approach to the aerodynamic identification of unstable aircraft , 1991 .

[6] A. Bryson,et al. PARAMETER IDENTIFICATION OF LINEAR SYSTEMS BASED ON SMOOTHING , 1990 .

[7] Moshe Idan,et al. Nonlinear smoothing identification algorithm with application to data consistency checks , 1993 .

[8] P. Khargonekar,et al. Filtering and smoothing in an H/sup infinity / setting , 1991 .

[9] Robert F. Stengel,et al. Determination of nonlinear aerodynamic coefficients using the estimation-before-modeling method , 1988 .

[10] R. V. Jategaonkar,et al. Identification of Actuation System and Aerodynamic Effects of Direct-Lift-Control Flaps , 1993 .

[11] K. W. Iliff,et al. Parameter Estimation for Flight Vehicles , 1989 .