壳体材料对地磁传感器测量弹体转速的影响

为消除弹丸壳体材料对地磁传感器测量弹体转速时采集数据的影响,分析了地磁传感器测量弹体转速的原理和数据采集电路的组成.采用铝壳材料和钢壳材料作为弹丸壳体进行数据采集,通过对采集数据的分析,获得了铝壳材料和钢壳材料对采集数据的影响参数.     

基于反电动势的多相感应电机MRAS控制策略优化

针对舰用多相电力推进系统无速度传感器控制的需求,将带输入滤波环节的基于电机反电动势的模型参考自适应(MRAS)方法用于多相感应电机无速度传感器矢量控制系统,推导了系统的小信号模型,分析了滤波截止频率和转速估算PI参数对系统性能的影响,并在此基础上设计了变滤波截止频率变PI参数优化的MRAS控制策略。仿真和实验结果表明:该优化方法具有更高的转速估算精度和静、动态控制性能。     

装甲车辆起动电动机综合试验台

采用较先进的磁粉制动器作为电机的负载,使电机加载平稳、可靠、恒定,并可连续调节负载大小;同时采用高精度的ZJ型转矩转速传感器并配合转矩转速仪,不但能测量电机稳态时的转矩、转速和功率,同时还可测试电机某一过渡过程中转矩、电流、转速随时间变化的数值并贮存或打印.     

基于定子反电势E的异步电机速度辨识方法

针对以转子磁通作中间变量 ,利用定子电压电流辨识电机转速的MRAS方法存在的问题 ,提出以反电势作中间变量的改进的MRAS转速辨识方法 .通过对无速度传感器矢量控制系统的仿真 ,表明该方案具有较好的实用性     

内燃机瞬时转速测量干扰因素分类与仿真

将影响内燃机瞬时转速测量的因素分为调频、调幅和附加波形影响,并得到了在这些干扰下磁电式传感器输出电压波形的理论函数表达式;使用插值计数法分别对3类因素的影响进行了仿真,结果证明了附加波形对瞬时转速测量计算的影响最大,调频干扰次之,调幅干扰对其几乎没有影响.     

军用车辆轮毂电机位置传感器故障检测及容错控制

针对电传动装甲车辆恶劣工况下轮毂电机位置传感器容易产生故障问题,基于脉振高频电压注入法构建了位置传感器故障检测及容错控制系统.通过分析故障时位置传感器输出信号出现的幅值不平衡故障或正交不完全故障,采用阈值检测法实现故障检测,并使电机由有位置传感器控制切换为无位置传感器控制.仿真及实验结果表明,故障发生时,系统能够迅速检测出故障并进行容错控制,有效抑制了电机转速及定子电流的持续振荡.     

新型管压传感器的研制及应用

针对目前外卡式管压传感器存在的问题，设计制作了一种新型外卡式ICP（Integrated Circuit Piezoelectric）型管压传感器。利用该传感器采集了柴油机高压油管压力信号，通过对测试信号的无延时实时滤波、去趋势项和归一化处理，实现了柴油机转速的准确计算；通过时域波形的分析，提取了4个喷油特征点。研究结果表明：该传感器具有使用方便、性能可靠和测试准确的特点。     

利用零交叉点测量旋转弹磁方位角的试验方法

针对旋转弹在地磁空间运动时的环境条件,提出了基于零交叉点原理测量弹体磁方位角的模拟试验方法,并在不同的方位角、传感器倾角和转速等条件下进行了试验.试验结果表明,零交叉点原理可以实现弹体在地磁场中的角度测量,精度基本控制在±3°的范围内,并可进一步减小误差,但该原理也存在测量盲区,盲区范围与传感器倾角有关.     

基于MRAS的感应电机无传感器控制策略优化

传统感应电机无传感器控制策略采用基于电压模型的转速辨识方法,存在积分初始值误差和直流偏置问题,从而影响转速跟踪效率和观测精度。针对这一问题,用滤波环节替代原有纯积分器并增加反馈补偿,提出了一种改进型基于转子磁链的模型参考自适应系统(MRAS)方法。在此基础上,通过MATLAB/SIMULINK平台搭建数学模型,对改进型基于转子磁链的MRAS法和传统MRAS法进行了仿真研究。仿真结果表明:改进型转子磁链MRAS法能够快速准确辨识电机转速,具有较强的鲁棒性和较好的动静态性能。     

电传动车辆轮毂电机无位置传感器控制研究

为提高电传动装甲车辆运行可靠性,提出一种基于脉振高频注入法进行转子位置辨识的轮毂电机控制策略。在永磁同步电机最大转矩电流比和弱磁控制的基础上,将位置辨识算法运用到控制系统并进行仿真分析。仿真结果表明:在电机起动加速阶段和转矩突变等工况下,该算法能够准确辨识出转子位置和电机转速,与使用传感器来获得转速的方式比较,基本能获得相同的控制效果,为进一步提高装甲车辆可靠性提供了可行方案。     

自行火炮发动机振动仿真研究

针对某型自行火炮柴油发动机系统,采用Matlab软件的Simulink 工具,建立了整个系统的动力学仿真模型。分别对该模型进行正弦、白噪声信号扰动下的仿真,从系统输出转矩和转速的曲线结果分析,证明了该模型具有较好的可信度。该模型的建立为今后深入开展发动机仿真研究提供了基础。     

机械运动参数的单片机测试系统

本文利用MCS-51单片机和白行设计的光栅式光电传感器构成了位移、速度、加速度测试系统,讨论了充分利用单片机软、硬件资源对光电传感器信号进行采集和处理的技巧,并对测试信号进行了软件抗干扰设计,系统测量范围是:位移>2mm,速度为0.0305～2000m/s,通过配用相应的传感器也可测量角运动信号,本系统已成功地应用于“轻武器后座参数综合测试仪”上,     

武器自动机光电测速技术研究

本文在科研样机研制的基础上,深入探讨了武器自动机光电测速系统的原理、设计思想及具体实现方法,对系统的主要技术指标进行了分析评估.     

A Measurement System for Railgun Test

A measurement system was designed to measure the railgun's parameters in launching process,which includes Rogowski coil sensor for measuring rail's current,B-dot probe for obversing projectile's velocity in bore,net target for catching muzzle velocity,signal condition circuit and high-speed data acquisition card for analyzing and storing data.Its software was also developed in WINDOWS operational environment via modularized design.The designed sensors and test software were successfully used in a practical electromagnetic railgun system to monitor the process of launching.The test results indicate that the state of launching can be intuitively observed and the parameters are accurately acquired and recorded.The software design method can shorten the development cycle,enhance the system's flexibility and provide the interface for the secondary development.The system shows great reliability.It is an effective and practical measurement platform for further research on the electromagnetic launch system.     

弹丸速度的数字化激光幕测试技术

针对传统弹丸速度测量方法的局限，提出一种新的弹丸速度测试技术——数字化激光幕结合互相关速度测量算法的测试技术，并给出了激光总体测速方案、测速原理以及互相关测速方法，经靶场试验验证测试效果良好。     

制式枪膛压测量方法研究

本文针对枪膛内压力变化的测量问题,提出将应变片直接粘贴在枪管外壁上测量其膛压,并根据厚壁圆筒理论,分析了该方法的可行性,同时,与压电式压力传感器进行了对比试验,结果表明,该方法简便可行,测量结果可靠。     

水池拖动模型阻力测量系统

介绍了以8031单片机为控制核心,由传感器、放大器、微型打印机及数据采集自动启动电路构成的阻力测量系统。它装在水池小型拖车上,能自动启动阻力测量,自动计算及打印结果,具有体积小、重量轻、自动化程度高、精度好等特点,有较好的实用价值。     

Ricochet quantification using a multiple sensor approach

This study investigates the ricochet behaviour of three different small-arms projectile types using a novel ricochet measuring device.The results can be used to estimate the danger potential of ricochets on shooting ranges.A ricochet is the change of direction and velocity of a projectile after impacting an oblique surface.This impact produces strong vibrations on a rigid plate.During this impact,flexural waves travel radially outwards from the point of impact.These waves are used to determine the properties of the impactor with accelerometers situated on the target surface.With the use of two measurement plates,one can produce a ricochet and detect the velocity at the same time.Accelerometers are suitable for accurate momentum measurements of single impacts.However,depending upon strike velocity and the impact angle,a ricochet can separate in multiple fragments after being deflected.From the operational safety perspective,these fragments need to be detected,as well.The approach of a coupled sensor concept was chosen to solve this problem.Thermographic sensors were additionally used to visualise the heat which is produced after pene-trating a rubber layer pasted in front of the steel target plate.With this approach one was able to detect the position of impact.The investigations showed that the measurement system performance is better with a multiple sensor design,which includes accelerometers for the velocity,impact strength and partly the position measurement,while the thermographic sensor was used for the position measurement and partly the momentum measurement.The investigated ammunition showed plausible fragmentation behaviour,and the results can already be used to estimate the danger potential of different ammunition types.Frangible projectiles fragment to small particles already after being deflected under a small angle.However,Full Metal Jacket projectiles with or without a steel core do not fragment under angles which are less than 5°.The objective of the paper is to demonstrate the possibility of measuring the complex ricochet me-chanics of small projectiles using standard accelerometers with the adequate signal processing approach.This measuring system is supported by an off the shelf thermographic camera.     

A novel launch dynamics measurement system for multiple launch rocket system and comparative analysis with numerical simulations

In this paper,a novel launch dynamics measurement system based on the photoelectric sensor pair is built.The actual muzzle time(i.e.a time duration that originates from the initial movement to the rocket's departure from the muzzle)and the muzzle velocity are measured.Compared with the classical methods,the actual muzzle time is obtained by eliminating the ignition delay.The comparative analysis method is proposed with numerical simulations established by the transfer matrix method for multibody systems.The experiment results indicate that the proposed measurement system can effectively measure the actual muzzle time and reduce the error of classical methods,which match well with the simulation results showing the launch dynamics model is reliable and helpful for further analysis and design of the MLRS.     

海用跟踪雷达轴线角速度测量

讨论了一种伺服设计方案的雷达轴线角速度的测量方法。给出了三个不同的测量点,并说明在稳态条件下,从这三个点测量到的结果都可当作目标视线角速度,且误差不大。最后还给出了测量值的暂态计算机模拟结果。