1) missile inertia device
导弹惯性器件
1.
According to design requirement of missile inertia device fault prediction system and the advantage of support vector machine(SVM).
文中针对导弹惯性器件故障预报系统的设计要求,考虑到支撑矢量机用于故障预报的优点,在导弹惯性器件的故障预报过程中应用了支撑矢量机的训练算法。
2) inertial device
惯性器件
1.
Fault prediction for inertial device based on LMBP neural network;
基于LMBP神经网络的惯性器件故障预报方法研究
2.
An orientation project based on inertial device was introduced in the paper.
介绍一种以惯性器件为基础的定位方案,与管道位置有关的检测信息存储在采集系统中,避免了外界环境的干扰,可以提高系统的可靠性、大大的减少了检测工作量与检测成本。
3.
The algorithm has been used in fault prediction of the inertial device of missile.
将此算法应用于导弹惯性器件故障预报中,通过实例证明了GNNM(3,1)模型对导弹武器故障预报的有效性。
3) Inertia device
惯性器件
1.
The prediction performances of the method are tested on simulation experiment of inertia device fault prediction.
文中将该方法应用于某飞行器惯性器件的故障预报当中并进行了仿真实验。
2.
To improve fault predicting precision,the signal energy spectrum in multi-wavelet domain was used as fault diagnosis characteristics,support vector machine (SVM) was used for fault prediction of inertia devices of missile.
利用训练后的SVM进行故障预报,试验结果表明多小波能量谱能更有效地反映惯性器件故障特征,利用SVM与多小波能量谱结合可以得到更好的预测精度。
4) inertial instrument
惯性器件
1.
According to the development of inertial instrument test platform,this paper presents the necessity of designing inertial instrument automatic test platform.
结合惯性器件测试平台的发展现状,指出了设计惯性器件自动测试平台的必要性,给出了测试平台的总体设计思想以及硬件和软件的设计。
5) inertial apparatus
惯性器件
1.
Fault monitoring and diagnosis of inertial apparatus based on time-frequency analysis pattern recognition;
基于时频分析和模式识别的惯性器件故障监测与诊断技术研究
2.
A method of fault diagnosis for the inertial apparatus based on Wavelet Packet is discussed.
提出了一种基于小波包分解的惯性器件故障检测与诊断方法,该方法利用小波包精确细分的特点,分别对正常系统和故障系统的观测信号进行小波包分解,提取其特征信息,从而实现对惯性器件的故障诊断。
6) inertial instruments
惯性器件
1.
This paper develops a set of auto-calibrating system for inertial instruments based on Acutronic two-axis turntable by using GPIB interface card, HP34401A multimeter, workstation and VC integration developing environment.
基于Acutronic双轴转台,采用GPIB接口卡、HP34401A数字万用表、计算机工作站及VC开发平台等,开发了一套惯性器件自动标定系统。
2.
Four project equations of object in two frames are established using inertial instruments measured attitude,then the least squared solution of relative height is deduced.
利用惯性器件测量的姿态角,建立了目标在2帧图像的4个投影方程,得到目标相对高度的最小二乘解。
补充资料：MX导弹(见“和平卫士”导弹)
MX导弹(见“和平卫士”导弹)
MX missile
MX daodanMx导弹(Mx mis、ix。)见“和平卫士”导弹。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条