Landing gears are one of the key components for large or middle unmanned aerial vehicles,and their working performances directly affect flying security and aircraft taking-off and landing performance.Thus,it is meanin...Landing gears are one of the key components for large or middle unmanned aerial vehicles,and their working performances directly affect flying security and aircraft taking-off and landing performance.Thus,it is meaningful to study the retraction system.Based on CATIA and ADAMS software platforms,a virtual model of landing gear retraction system is built for performance test,and then dynamic simulation is carried out.Afterwards,a test system for landing gear retraction is established,and the test data are compared with the results acquired from dynamics simulation.The main factors which affect the dynamic performance of retractable landing gear are analyzed emphatically.The simulation results show that aerodynamic load has an impact on retraction time,the mass force affects extension process,and the oil hole size of hydraulic actuator has an effect on both retraction time and extension time.展开更多
A new fluid bag buffer mechanism,which can provide large axial stiffness under the small displacement,is designed.The dynamic change laws of the mechanism stiffness and the internal pressure of the fluid bag are studi...A new fluid bag buffer mechanism,which can provide large axial stiffness under the small displacement,is designed.The dynamic change laws of the mechanism stiffness and the internal pressure of the fluid bag are studied when it is subjected to impact load.According to the protection performance for the flexible joint and the pressure change in the fluid bag during the impact process,the sensitivity of the geometric parameters of the fluid bag to the axial stiffness is analyzed by using the orthogonal experimental method,and the optimal parameter combination of the geometric parameters of the fluid bag under impact is obtained,leading to the displacement of the inner shell reduce by 41.4%.The results show that the internal pressure of the fluid bag is a rising process of oscillation and fluctuation.The sensitivity of the geometric parameters of the fluid bag to the displacement of the inner shell from high to low is as follows:Height H,radius r,wall thickness t,chamfer A.The correlation between the geometric parameters of the fluid bag and its internal pressure is:H is negatively correlated with the internal pressure,while the r,t,and A are positively correlated with the internal pressure.展开更多
针对混沌直接序列扩频(Chaotic Direct Sequence Spread Spectrum,CD3S)通信技术的实现问题,提出了一种CD3S通信的软件无线电实现方案,阐述了CD3S通信系统发收机的设计方法。发射机由软件实现信息码的混沌扩频,并通过硬件平台完成发射...针对混沌直接序列扩频(Chaotic Direct Sequence Spread Spectrum,CD3S)通信技术的实现问题,提出了一种CD3S通信的软件无线电实现方案,阐述了CD3S通信系统发收机的设计方法。发射机由软件实现信息码的混沌扩频,并通过硬件平台完成发射。接收机由硬件平台完成下变频与采样,然后通过软件实现定时同步、载波同步与信息解调。信息解调由多滤波器解调算法实现。在多滤波器解调算法中,由无损卡尔曼滤波(Unscented Kalman Filter,UKF)估计混沌码、卡尔曼滤波(Kalman Filter,KF)估计信道参数和最小均方误差(Minimum Mean Square Error,MMSE)滤波估计信息码这3个滤波器交替工作,通过联合估计实现信息码的解调。实验结果表明,该方案可以实现CD3S通信。展开更多
A new satellite to satellite passive tracking method using Bearings-Only measurements in Modified Spherical Coordinates(MSC) is proposed.The system dynamics and measurement process are presented in three-dimensional M...A new satellite to satellite passive tracking method using Bearings-Only measurements in Modified Spherical Coordinates(MSC) is proposed.The system dynamics and measurement process are presented in three-dimensional MSC,and then the tracking method is deduced in details based on the Cartesian method.Performance of the new method is validated through computer simulations,which proved that the proposed method is effective in terms of the estimation accuracy and convergence time compared with the Cartesian method no matter the Initial State Errors(ISE) and measurement errors are large or small.展开更多
文摘Landing gears are one of the key components for large or middle unmanned aerial vehicles,and their working performances directly affect flying security and aircraft taking-off and landing performance.Thus,it is meaningful to study the retraction system.Based on CATIA and ADAMS software platforms,a virtual model of landing gear retraction system is built for performance test,and then dynamic simulation is carried out.Afterwards,a test system for landing gear retraction is established,and the test data are compared with the results acquired from dynamics simulation.The main factors which affect the dynamic performance of retractable landing gear are analyzed emphatically.The simulation results show that aerodynamic load has an impact on retraction time,the mass force affects extension process,and the oil hole size of hydraulic actuator has an effect on both retraction time and extension time.
基金supported by the Fun⁃damental Scientific Research Business Expenses of Central Universities(No.NJ2020024).
文摘A new fluid bag buffer mechanism,which can provide large axial stiffness under the small displacement,is designed.The dynamic change laws of the mechanism stiffness and the internal pressure of the fluid bag are studied when it is subjected to impact load.According to the protection performance for the flexible joint and the pressure change in the fluid bag during the impact process,the sensitivity of the geometric parameters of the fluid bag to the axial stiffness is analyzed by using the orthogonal experimental method,and the optimal parameter combination of the geometric parameters of the fluid bag under impact is obtained,leading to the displacement of the inner shell reduce by 41.4%.The results show that the internal pressure of the fluid bag is a rising process of oscillation and fluctuation.The sensitivity of the geometric parameters of the fluid bag to the displacement of the inner shell from high to low is as follows:Height H,radius r,wall thickness t,chamfer A.The correlation between the geometric parameters of the fluid bag and its internal pressure is:H is negatively correlated with the internal pressure,while the r,t,and A are positively correlated with the internal pressure.
文摘A new satellite to satellite passive tracking method using Bearings-Only measurements in Modified Spherical Coordinates(MSC) is proposed.The system dynamics and measurement process are presented in three-dimensional MSC,and then the tracking method is deduced in details based on the Cartesian method.Performance of the new method is validated through computer simulations,which proved that the proposed method is effective in terms of the estimation accuracy and convergence time compared with the Cartesian method no matter the Initial State Errors(ISE) and measurement errors are large or small.
