Validation of the Dynamic Response of a Blade-Element UH-60 Simulation Model in Hovering Flight
暂无分享,去创建一个
[1] Wayne Johnson,et al. Influence of unsteady aerodynamics on hingeless rotor ground resonance , 1982 .
[2] Mark B. Tischler,et al. Frequency-Response Method for Rotorcraft System Identification: Flight Applications to BO 105 Coupled Rotor/Fuselage Dynamics , 1992 .
[3] Robert T. N. Chen. A survey of nonuniform inflow models for rotorcraft flight dynamics and control applications , 1990 .
[4] Mark G. Ballin. Validation of a real-time engineering simulation of the UH-60A helicopter , 1987 .
[5] Mark B. Tischler,et al. Advancements in frequency-domain methods for rotorcraft system identification , 1988 .
[6] F J Bailey. A simplified theoretical method of determining the characteristics of a lifting rotor in forward flight , 1941 .
[7] M. A. Diftler,et al. Helicopter Simulation Development By Correlation With Frequency Sweep Flight Test Data , 1989 .
[8] Mark G. Ballin,et al. A high fidelity real-time simulation of a small turboshaft engine , 1988 .
[9] Mark B. Tischler,et al. Time and Frequency-Domain Identification and Verification of BO 105 Dynamic Models , 1991 .
[10] Mark B. Tischler,et al. Frequency-response identification of XV-15 tilt-rotor aircraft dynamics , 1983 .
[11] David A. Peters,et al. Review of dynamic inflow modeling for rotorcraft flight dynamics , 1986 .
[12] Xin Zhao,et al. A linearized model of helicopter dynamics including correlation with flight test , 1988 .