误差角的英文

• error angle

• "误差"英文翻译    error
• "角"英文翻译    role; part; character
• "雷达误差角" 英文翻译 :    radar error angle
• "临界误差角" 英文翻译 :    critical error angle
• "陀螺误差角" 英文翻译 :    gyro error angle
• "垂直循迹误差角" 英文翻译 :    vertical tracking angle error
• "横向循迹误差角" 英文翻译 :    lateral tracking angle error
• "雷达方位误差角" 英文翻译 :    target radar azimuth error angle
• "差角" 英文翻译 :    angle of difference; declinate
• "偏差角,自差角" 英文翻译 :    angle of deviation
• "差角法" 英文翻译 :    angle-offset method
• "磁差角" 英文翻译 :    angle of variation; declinate
• "航差角" 英文翻译 :    drift angle
• "偏差角" 英文翻译 :    angle of deviation; deflection; deflexion; deviation angle; drift angle
• "平差角" 英文翻译 :    adjust angle; adjusted angle
• "色差角" 英文翻译 :    hue-difference angle
• "视差角" 英文翻译 :    angle of parallax; parallactic angle = position angle; parallax angle; subtense angle
• "位差角" 英文翻译 :    shift angle
• "象差角" 英文翻译 :    angle of aberration
• "翼差角" 英文翻译 :    decalage
• "单眼视差角" 英文翻译 :    monocular parallactic angle
• "风的偏差角" 英文翻译 :    inclination of the wind
• "风流压差角" 英文翻译 :    leeway angle
• "风压差角" 英文翻译 :    angle of leeway; leeway angle
• "光行差角" 英文翻译 :    aberration angle

• Vertical tracking angle error
  垂直循迹误差角
• It has made experiment detection and rectification with signal control technology for the position signal error
  利用数字控制技术对位置信号误差角进行了实验检测及校正。
• This paper studied zero - velocity correct technology for ins , based on analysis of ins error equation , it concluded the method by which we can use ins velocity output to estimate the attitude angle error when the vehicle halted , then it contrasted two schemes of conic approximation of attitude angle error and put forward a method to decide the approximation coefficient by time range
  本文首先研究了车载捷联惯导系统( ins )的零速修正技术，在分析捷联惯导系统误差方程特点的基础上，推导了停车时利用ins速度输出估计姿态误差角的方法，并对用二次曲线拟合姿态误差角的两种方案作了比较，提出了按时间分段确定拟合系数的方法。
• The mechanisms and conditions for the mechanisms to adjust itself were analyzed in detail . an accurate method of analyzing for the properties of the mechanisms without overconstraints was given for the first time , we obtained the equations of self - adjusting displacement in the cylindrical pair , the allowable kinematic - pair - axis errors which enable the mechanisms realize function of self - adjustment , and the most rational arrangements of kinematic pairs for the three common four - bar mechanisms . the results of analysis show that the influences of the errors of crank - pin on the self - adjusting properties of the mechanisms are bigger than that of the other pairs
  ( 3 )详细分析了无过约束机构能够实现自调的机理及机构能够实现自调的条件，首次提出了无过约束机构自调性分析的一种精确方法，得到机构自调时圆柱副中的自调位移规律和机构能够实现自调的运动副允许误差角以及三种常用平面四杆机构的自调结构的最适宜的运动副配置方式。