Zobrazeno 1 - 10
of 12
pro vyhledávání: '"Shi Xing Zhu"'
Publikováno v:
Applied Mechanics and Materials. 779:239-243
The LQR controller is designed to control magnetorheological damper through controlling the output damping force of magnetorheological damper. Simulation models of LQR controller is built. The results of LQR models and simulation model of landing gea
Publikováno v:
Applied Mechanics and Materials. 779:212-219
The semi-active control of MR damper is established, using a simplified model of landing gear system and DSP2812 as the code control board. The fuzzy control system is created based on software fuzzyTECH and simulation mode was established in matlab\
Publikováno v:
Applied Mechanics and Materials. 779:226-232
For characteristics of nonlinearity and time-varying volatility of landing gear based on MR damper, a BP neural network PID controller with a momentum was designed on basis of established dynamic mathematical model. BP neural network would adjust thr
Autor:
Shi Xing Zhu, Jian Hai Xue
Publikováno v:
Applied Mechanics and Materials. :626-632
Design of a new magnetorheological damper gap structure, combined with viscous lag model, analyzed the damper structural parameters, Design the damping devices with different sizes. Comparison of the structure of the damper with different sizes after
Publikováno v:
Applied Mechanics and Materials. 665:601-606
The structure of a shock absorber based on magnetorheological (MR) damper with a metering pin is proposed, and structure of the magnetic circuit of MR damper is optimized. By drop tests, the damping characteristics of the shock absorber and damping e
Autor:
Chan Juan Chen, Shi Xing Zhu
Publikováno v:
Applied Mechanics and Materials. 233:66-71
Aircraft landing gear shock system model was established, The system vibration differential equation and state-space equation were deserved。Based on the general fuzzy PID controller, the idea of fuzzy PID controller and its application in shock abs
Autor:
Zhi Ni Ren, Shi Xing Zhu
Publikováno v:
Advanced Materials Research. 505:489-493
In order to reveal the science of adding winglet for Active aircraft, the paper calculates the aerodynamic efficiency of a wing added winglet using CFD technology, Aerodynamic benefit of the wing added winglet reaches the maximum when the angle of at
Publikováno v:
Advanced Materials Research. :1481-1485
Modeling of a multi- ring grooves Magnetorheological(MR)fluid damper designed by ourselves were respectively carried out based on the Bingham model and the Herschel-Bulkley model. By comparing the simulation results of the two models with the tru
Publikováno v:
Mechanics and Mechatronics (ICMM2015).
Publikováno v:
Proceedings of the 2015 International Conference on Industrial Technology and Management Science.