基于LQR直升机模糊滑模跟踪控制

研究直升机系统稳定性优化问题,由于直升机系统的强耦合和非线性特性的影响,使飞行的稳定性和实时跟踪性差。为解决上述问题,对直升机原始数学模型进行近似线性化和解耦处理,采用模糊滑模控制方法实现直升机姿态角度的跟踪控制。首先,在滑模面的设计中引入最优线性二次型调节器,构建一种积分型切换面。其次,以切换面及导数的乘积和滑模切换增益的变化量为模糊系统的变量,实时调整变结构控制项的切换增益。仿真结果表明,通过控制器设计能够实现直升机姿态角度跟踪的稳定性,对外界不确定干扰具有强鲁棒性且控制器输出抖振问题得到明显改善。     

基于环状电极的电容式润滑油磨粒检测系统设计

摩擦副非正常磨损时将产生直径为几十微米的大金属磨粒。采用阻抗类方法检测磨粒时,要求传感器具有较高的灵敏度。为此,设计了差分结构的环状极板电容式传感器。应用电容/数字转换芯片AD7746将传感器的输出直接转换为数字信号,省去了前端复杂的信号调理电路,简化了设计,并且有效地降低了寄生电容和杂散电容的影响。实验表明:系统分辨率可以达到0.125 fF,极大提高了系统灵敏度。     

基于物联网的航空物流查询平台

针对国内航空物流信息化建设方面的问题,提出并设计了一套基于物联网的航空物流查询系统。该系统通过RFID技术完成数据采集,并通过RS232串口将数据传输到ZigBee终端节点,然后利用ZigBee无线网络进行短距离传输到路由节点,最后经过 ZigBee 网关将信息传输出去。实验结果表明该平台可以对航空货物进行智能化、可视化、信息化管理。该设计为航空物流管理提供了新的思路,有良好的应用前景。     

Hierarchical control for cornering stability of dual-motor RWD vehicles with electronic differential system using PSO optimized SOSMC method

This paper proposes a novel control scheme with a three-layer hierarchical structure to improve the cornering stability of the dual-motor rear-wheel drive (RWD) vehicles with the electronic differential system (EDS). The proposed hierarchical structure for the control system includes the observing layer, control layer, and actuation layer. In the observing layer, the driver model is designed to obtain the nominal steering angle, and the state observer is designed to obtain the yaw angle which cannot be easily measured. Then, particle swarm optimization (PSO) and second order sliding mode control (SOSMC) are employed in the control layer. The SOSMC part is used to design the control law to eliminate the chattering problem in the sliding mode algorithm, and the PSO part is used to obtain the optimal weights in the sliding mode surface to meet the minimum sideslip angle error and yaw rate error. The actuation layer allocates the corrected yaw moment by distributing the driving force to each independent driving wheel. Finally, the numerical tests are carried out under the double line change (DLC) maneuver. The results show that the proposed control system can effectively improve the cornering stability of the dual-motor RWD vehicles and reduce their motor power consumption.     

一种改进的高精度组合导航滤波算法仿真

在INS/GPS组合导航系统的研究中,为了解决非线性滤波算法在系统模型不确定情况下出现的滤波精度低、鲁棒性差的问题,提出了一种将强跟踪滤波算法与容积卡尔曼滤波算法(CKF)相结合的组合导航滤波算法(SMFCKF).SMCKF算法将强跟踪滤波算法中的多重次优渐消因子引入到CKF算法的状态预测协方差矩阵中,对不同的状态通道进行相应的渐消.通过建立INS/GPS组合导航系统的非线性模型,对改进的滤波算法进行仿真,结果表明改进的滤波算法提高了滤波精度和鲁棒性,滤波效果优于CKF算法,适合应用于INS/GPS组合导航系统中,为飞行器组合导航优化提供了参考.     

航空多芯电缆检测系统设计

介绍了航空多芯电缆通断测试、耐压绝缘阻值测量和漏电故障检测的原理和方法,并采用凌阳SPCE061A单片机和CPLD系统相结合,设计出一种实现对航空多芯电缆进行准确、高效、便捷测量的系统.该系统可快速对航空多芯电缆进行离线检测,准确测量电缆的通断、耐压绝缘阻值和电缆漏电点距离, 并实时显示测试结果.系统具有操作简单,运行可靠,测试精度高等特点.设计完成后经调试与运行,系统工作效果良好,并能准确实现各项电缆测试.     

Adaptive fault-tolerant control of linear systems with actuator saturation and L_2-disturbances

This paper studies the problem of designing adaptive fault-tolerant H-infinity controllers for linear timeinvariant systems with actuator saturation.The disturbance tolerance ability of the closed-loop system is measured by an optimal index.The notion of an adaptive H-infinity performance index is proposed to describe the disturbance attenuation performances of closed-loop systems.New methods for designing indirect adaptive fault-tolerant controllers via state feedback are presented for actuator fault compe...     

Prediction of stable high-pressure structures of tantalum nitride TaN2

Structure searches based on a combination of first-principles calculations and a particle swarm optimization technique unravel two new stable high-pressure structures (C2/m and Cmce) for TaN₂. The structural features, mechanical properties, formation enthalpies, electronic structure, and phase diagram of TaN₂ are fully investigated. Being mechanically and dynamically stable, the two phases could be made metastable experimentally at ambient conditions.     

基于阵列涡流技术的裂纹特征量研究

阵列涡流传感器能够实现导电材料的大面积高速扫描。不同走向的裂纹对线圈间互感的影响是不同的,因此,测量线圈间的互感能够获得更多的缺陷信息。利用ANSYS软件对横向和纵向裂纹进行了三维有限元仿真,得到了相应的阵列涡流敏感线圈感应电动势幅值变化曲线。仿真结果表明:通过测量线圈间的互感,可以实现对裂纹长度和方向等特征量的检测。