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- W2892491749 abstract "In order to solve the vibration problem of the tail plane on a certain aircraft appears in ground test, on the basis of analyzing the system's control structure, modeling the booster and the mechanical transmissions. The support stiffness of the tail plane's actuator, the joint stiffness of piston and load, the connection stiffness of the mechanical transmission parts and the nonlinear links are all taken into account in the modeling process. Simulation results show that the support stiffness of the actuator cylinder has great influence on the stability of the system. When the stiffness is small, the surface rudder of tail plane vibrates without attenuation, and the vibration frequency is large, after the stiffness is increased the vibration attenuates soon. The simulation results and the experimental results are basically identical. On the basis of the simplified mathematical model analyze the system's stability in theory which illustrates the mechanism of support stiffness on the stability of the system." @default.
- W2892491749 created "2018-10-05" @default.
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- W2892491749 date "2018-05-01" @default.
- W2892491749 modified "2023-09-26" @default.
- W2892491749 title "Optimization Analysis of Control Plane on Tail Plane" @default.
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- W2892491749 doi "https://doi.org/10.1109/imcec.2018.8469643" @default.
- W2892491749 hasPublicationYear "2018" @default.
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