Identification of nonlinear helicopter rotor structural dynamics
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[1] F. Nitzsche,et al. MODAL SENSORS AND ACTUATORS FOR INDIVIDUAL BLADE CONTROL , 1993 .
[2] Khanh Q. Nguyen,et al. Higher harmonic control analysis for vibration reduction of helicopter rotor systems , 1994 .
[3] Kurt H. Hohenemser,et al. Identification of state variables and dynamic inflow from rotor model dynamic tests , 1977 .
[4] M. Borri,et al. Helicopter rotor dynamics by finite element time approximation , 1986 .
[5] Richard Bellman,et al. Quasilinearization and the Identification Problem , 1983, Series in Modern Applied Mathematics.
[6] Firdaus E. Udwadia,et al. A Methodology for Optimal Sensor Locations for Identification of Dynamic Systems , 1978 .
[7] Frederick Tasker,et al. Extended variance-based techniques for sensor location in modal identification , 1994 .
[8] J. Chow,et al. A trajectory sensitivity method for the identification of nonlinear excitation system models , 1993 .
[9] W. R. Witkowski,et al. Approximation of parameter uncertainty in nonlinear optimization-based parameter estimation schemes , 1993 .
[10] John L. McCloud,et al. A Numerical Simulation Study of Open‐Loop, Closed‐Loop and Adaptive Multicyclic Control Systems , 1983 .
[11] Paolo Mantegazza,et al. Basic features of the time finite element approach for dynamics , 1991 .
[12] D. Peters,et al. hp-version finite elements for the space-time domain , 1988 .