Parameter Identification of Spin-Stabilized Projectiles Using a Modified Nowton-Raphson Minimization Technique
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[1] E. Dowell. Comment on "Direct Solutions for Strum-Liouville Systems with Discontinuous Coefficients" , 1980 .
[2] D. B. Kirk,et al. A Method for Extracting Aerodynamic Coefficients from Free-Flight Data , 1969 .
[3] Y. Chen,et al. Drag coefficient curve identification of projectiles from flight tests via optimal dynamic fitting , 1997 .
[4] R. K. Mehra,et al. Maximum likelihood identification and optimal input design for identifying aircraft stability and control derivatives , 1973 .
[5] Mingxuan Sun,et al. High-order iterative learning identification of projectile's aerodynamic drag coefficient curve from radar measured velocity data , 1998, IEEE Trans. Control. Syst. Technol..
[6] R. V. Jategaonkar,et al. Algorithms for aircraft parameter estimation accounting for process and measurement noise , 1989 .
[7] K. W. Iliff,et al. Determination of stability derivatives from flight data using a Newton-Raphson minimization technique , 1972 .
[8] R. E. Maine,et al. Application of parameter estimation to aircraft stability and control: The output-error approach , 1986 .