Dynamic Strain Measurement of Rotor Blades in Helicopter Flight Using Fiber Bragg Grating Sensor von Zhang, Honglin, Wang, Zefeng, Teng, Fei, Xia, Pinqi

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Active Vibration Control of Helicopter Fuselage with Large Dynamic Modeling Errors von Kai, Lang, Lina, Shang, Pinqi, Xia

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An excellent harmonic feedforward-sliding mode output feedback hybrid algorithm for helicopter active vibration control von Lang, Kai, Shang, Lina, Xia, Pinqi, Song, Laishou

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Measurement Technique and Result Analysis of Helicopter Rotor Blade Structural Vibration Load von Zhang, Honglin, Wang, Zefeng, Xia, Pinqi

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Conceptual Assessment of New Helicopter Project Solutions Based on the Take-off Mass Sensitivity Analysis von Pinqi Xia, Kretov, A. S.

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An improved PSO algorithm for parameter identification of nonlinear dynamic hysteretic models von Zhang, Junhao, Xia, Pinqi

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MIMOMH feed-forward adaptive vibration control of helicopter fuselage by using piezoelectric stack actuators von Meng, De, Xia, Pinqi, Song, Laishou

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Active Control of Helicopter Structural Response Using Piezoelectric Stack Actuators von Song, Laishou, Xia, Pinqi

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Novel Modeling and Vibration Analysis Method on a Helicopter Drive Train System von Wang, Xiao, Xia, Pinqi

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Aeroelastic stability of full-span tiltrotor aircraft model in forward flight von LI, Zhiquan, XIA, Pinqi

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Aeroelastic stability of wing/pylon/rotor coupled system for tiltrotor aircraft in forward flight von Yang, ChaoMin, Xia, PinQi

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Analysis of energy conversion in two-mode vibration control using synchronized switch damping approach von Ji, Hongli, Qiu, Jinhao, Xia, Pinqi

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Geometrically Exact Aeroelastic Stability Analysis of Composite Helicopter Rotor Blades in Hover by Updated VABS von Shang, Lina, Xia, Pinqi

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Finite element corotational formulation for geometric nonlinear analysis of thin shells with large rotation and small strain von Yang, JinSong, Xia, PinQi

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Modeling and Optimal Control of Piezoactuated Rotating Box Beams with Sophisticated Couplings von Wang, Xiao, Xia, Pinqi

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Control of dynamic stall of helicopter rotor blades von Wang, Rong, Xia, PinQi

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Energy conserving and decaying algorithms for corotational finite element nonlinear dynamic responses of thin shells von Yang, JinSong, Xia, PinQi

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Rotation vector and its complement parameterization for singularity-free corotational shell element formulations von Yang, Jinsong, Xia, Pinqi

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Active Global Vibration Control of Helicopter Fuselage von Lang, Kai, Xia, Pinqi, Wang, Xiao

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The influence of switching phase and frequency of voltage on the vibration damping effect in a piezoelectric actuator von Ji, Hongli, Qiu, Jinhao, Xia, Pinqi, Guyomar, Daniel

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