多输入多输出电磁矢量阵列雷达的DOD和DOA联合估计

研究一种基于电磁矢量传感器阵列的多输入多输出(MIMO)雷达目标波离角(DOD)和波达角(DOA)的联合估计算法.提出了一种新型MIMO雷达系统,发射阵列采用常规阵元,而接收阵列采用电磁矢量传感器,在此基础上,算法首先利用矢量传感器的内在结构特点结合子空间旋转不变性质获得目标DOA预估计,随后采用最佳加权子空间拟合算法...     

Composite impact vector control based on Apollo descent guidance

A new three-dimensional missile guidance law to control the impact vector against a stationary target is proposed. The composite guidance law has two well-known components: Apollo descent guidance and trajectory shaping guidance. These respectively linear and planar guidance laws are combined to achieve a specified impact direction. The main idea is to define an impact plane and to steer the missile onto this plane using Apollo descent guidance while concurrently performing trajectory shaping wi...     

基于气隙磁场定向的无轴承异步电机非线性解耦控制

无轴承异步电机是一个强耦合的非线性复杂系统，实现了其电磁转矩和径向悬浮力之间的解耦控制是该电机稳定运行的前提。本在研究电机磁悬浮机理的基础上，提出了利用气隙磁场定向控制来实现两之间的动态解耦控制。仿真实验也证明该控制算法不仅能实现电机稳定的悬浮，而且使电机具有良好的调速性能。     

双 Y移 30°永磁同步电动机串联系统的仿真

双Y移30°永磁同步电动机串联系统可以实现同一变频电源供电和同一套控制平台下2台电机的解耦运行,节省了控制装置和外围电路,降低控制系统的体积、重量与成本。文章给出了双Y移30°永磁同步电动机串联系统的矢量控制策略,建立了仿真数学模型,并进行了变负载运行的仿真,结果验证了该串联系统解耦运行的可行性。     

Auto-normalization algorithm for robotic precision drilling system in aircraft component assembly

A novel approach is proposed to detect the normal vector to product surface in real time for the robotic precision drilling system in aircraft component assembly, and the auto-normalization algorithm is presented based on the detection system. Firstly, the deviation between the normal vector and the spindle axis is measured by the four laser displacement sensors installed at the head of the multi-function end effector. Then, the robot target attitude is inversely solved according to the auto-normalization algorithm. Finally, adjust the robot to the target attitude via pitch and yaw rotations about the tool center point and the spindle axis is corrected in line with the normal vector simultaneously. To test and verify the auto-normalization algorithm, an experimental platform is established in which the laser tracker is introduced for accurate measurement. The results show that the deviations between the corrected spindle axis and the normal vector are all reduced to less than 0.5°, with the mean value 0.32°. It is demonstrated the detection method and the auto-normalization algorithm are feasible and reliable.     

MULTI-CONTROLLER STRUCTURE OF SUPERMANEUVERABLE AIRCRAFT

Supermaneuver flight is often operated withhigh angle- of- attack and high angular rates.Su-per- maneuver flight cannot be controlled by aconventional gain- scheduled controller but canbe controlled by using a nonlinear dynamic- in-version controller[1～ 3] .　　 This paper presents a method to use twokinds of controllers,nonlinear dynamic- inver-sion and conventional gain- scheduled con-trollers,in a flight control system.The nonlin-ear dynamic- inversion controller is used to con-trol superm…     

Space debris mitigation in geosynchronous orbit

In order to preserve the geosynchronous region, the Inter-Agency Space Debris Coordination Committee (IADC) proposed and endorsed a re-orbiting strategy for spacecraft at the end-of-life: they should be disposed above the synchronous altitude and passivated, to reduce the risk of inadvertent explosions. The recommended perigee altitude of the disposal orbit took into account all relevant perturbations and was a function of the expected perturbing acceleration induced by solar radiation pressure. It was intended to prevent any further interference with a properly defined geostationary protected region.     

刀具角度分析与计算的矢量方法

刀具技术是机械制造工业的基础与支柱，刀具角度的分析与计算是刀具技术中关键技术问题之一。提出分析与计算刀具角度的矢量方法，概述矢量基本知识，阐述刀具角度的矢量法基本原理及其应用，以适应刀具技术发展之需要。     

基于大功率模块化多电平并网变流器的 永磁直驱风力发电系统矢量控制方法研究

进行了模块化多电平变流器（Modular Multilevel Converter,MMC） 电路拓 扑结构分析,对其工作状态原理进行阐述。将MMC 电路拓扑应用到永磁直驱风力发电 系统,使用基于电容电压排序的矢量控制作为逆变器控制策略。通过仿真软件搭建所述 系统,仿真结果证实了控制方式的可行性。     

Experiment of gas plasma plume deflection by magnetic control

To investigate the deflection effect of gas plasma plume controlled by magnetic field, a novel experimental scheme was presented. The Cs2CO3 catalytic ionization seeds were injected into the combustion chamber to obtain gas plasma on a high temperature magneto hydrodynamic (MHD) experiment rig. The plasma jet was deflected under the action of an external magnetic field, resulting in a thrust-vector effect. Particle image velocimetry (PIV) collected two-dimensional images of jet flow field. Through image processing and velocity vector analysis, the jet deflection angle can be obtained quantitatively. At 1800-2500K, the jet deflection was verified experimentally under the condition of 0.45T magnetic field strength. The results indicate that the jet deflection angle increases gradually with the increase of gas temperature, and above 2200K, the jet deflection angle increase obviously. In the process of gas plasma jet, it is feasible to realize the jet deflection controlled by MHD by adding an external magnetic field.