探讨指数波响应应用于冲击测量系统的问题。
Application of exponential wave response to impulse measuring systems is discussed.
本文介绍了一种根据冲击测量系统的方波响应和输出波形，利用FFT算法重建输入波形的方法。
This paper presents the input voltage shape reconstructed by FFT method from the distorted output shape and unit step response of impulse high voltage measuring system.
冲击过程中的接触载荷由压力传感器及数字信号处理系统实时测量。
The contact force during impact process was measured by force sensor and data signal processing system in real time.
使用该系统，可以很方便地测量冲击器的能量、频率、流量等重要指标。
It is very convenient for gauging the energy, frequency and flow of hydraulic shock device.
根据冲击电流计测直螺线管磁场的实验电路原理，利用数值计算方法，对减少测量的系统误差进行了理论分析。
According to circuit principle of the experiment of measuring magnetic field in straight solenoid by impact galvanometer, theory analysis on reducing system error is done by using numerical method.
介绍了一种变压器冲击试验测量分析系统的功能及工作原理。
The function and working principle of a digital analytic system for transformer impulse test measurement are introduced.
该系统能完成所要求的正弦振动实验、随机振动实验和冲击测量实验。
The system can finished the required functions of sine vibration experiment, randomicity vibration experiment and impact measurement experiment.
电力系统冲击接地电阻的测量是关系到电力系统稳定运行和电气设备安全的重要问题。
The measurement of grounding resistance under impulse voltage is of great importance for safe operation of power system and electronic equipment.
研究建立一种光学记录速度干涉仪系统(OR VIS)，用于激光产生冲击波研究物质状态方程实验中的参数测量。
An optically recording velocity interferometer system (ORVIS) is constructed. It is applied to laser-driven shock experiments as a method for equation of state (EOS) measurement.
新的国际标准体系中提出以认证、比对的手段考核冲击电压测量系统的不确定度。
The uncertainty of impulse voltage measurement as a checking means for authentication and comparison is suggested in the new international standard system.
目的测定在固定支撑和有缓冲器支撑方式下两种假人对系统着陆冲击的响应；检验人椅系统内冲击测量位置的设置是否正确。
Objective to quantify the response of human-chair system during landing impacts, and to testify the detecting position for system impact tests.
结果表明计程仪的测量误差会造成机动条件下惯导系统的冲击误差。
The result showed that log error may lead to impulsive errors of INS while the ship is maneuvering.
密封构件(104)的提供使得该系统较少受到冲击力的影响并降低了由于测量室(300)中的空气导致测量缺陷的风险。
The provision of the sealing member (104) renders the system less vulnerable to force impacts and reduces the risk of flawed measurements due to atmospheric air in the measuring chamber (300).
密封构件(104)的提供使得该系统较少受到冲击力的影响并降低了由于测量室(300)中的空气导致测量缺陷的风险。
The provision of the sealing member (104) renders the system less vulnerable to force impacts and reduces the risk of flawed measurements due to atmospheric air in the measuring chamber (300).
应用推荐