Parameter Estimation from Flight Data of an Unstable Aircraft Using Neural Networks
暂无分享,去创建一个
[1] L. Librescu,et al. Nonclassical effects on divergence and flutter of anisotropic swept aircraft wings , 1996 .
[2] Pong-Jeu Lu,et al. Flutter analysis of cantilever composite plates in subsonic flow , 1989 .
[3] Ajoy Kanti Ghosh,et al. Estimation of Aircraft Lateral-Directional Parameters Using Neural Networks , 1998 .
[4] I Lee,et al. Transonic Steady And Unsteady Aerodynamics For Wings Using Three Dimensional Euler Equations , 2001 .
[5] Prem Kalra,et al. Two new techniques for aircraft parameter estimation using neural networks , 1998, The Aeronautical Journal (1968).
[6] T. Weisshaar. Aeroelastic Tailoring of Forward Swept Composite Wings , 1981 .
[7] I. Lottati,et al. Flutter and divergence aeroelastic characteristics for composite forward swept cantilevered wing , 1985 .
[8] In Lee,et al. Transonic and supersonic flutter characteristics of a wing-box model with tip stores , 2001 .
[9] David K. Schmidt,et al. Flight dynamics of aeroelastic vehicles , 1988 .
[10] V. B. Venkayya,et al. Aeroelastic Tailoring of Composite Structures , 1999 .
[11] R. V. Jategaonkar,et al. Evaluation of Parameter Estimation Methods for Unstable Aircraft , 1994 .
[12] In Lee,et al. Transonic and Low-Supersonic Aerodynamic Analysis of a Wing with Underpylon/Store , 2000 .