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- W2372495360 abstract "This paper described an important character of helicopter control system:the characteristic of dynamic stiffness.The structures of helicopter control system were analyzed,and the mechanics model and mathematics model were set up.The formula of dynamic stiffness was deduced.Mechanical impedance method was applied to calculate dynamic stiffness on some type helicopter control system.The test data were compared with the calculation one,which demonstrated the exactness of the mechanics model and the effectiveness of the methods for calculating dynamic stiffness." @default.
- W2372495360 created "2016-06-24" @default.
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- W2372495360 date "2010-01-01" @default.
- W2372495360 modified "2023-09-23" @default.
- W2372495360 title "The Characteristic Research of Dynamic Stiffness on Helicopter Flight Control System" @default.
- W2372495360 hasPublicationYear "2010" @default.
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