误差方程的英文

• error equation
• errors equation

• "误差"英文翻译    error
• "方程"英文翻译    equation
• "误差方程式" 英文翻译 :    error equation
• "观测方程（又称“误差方程”）" 英文翻译 :    observation equation
• "内擂误差方程式" 英文翻译 :    error equation for interpolating
• "观测方程 观察方程 误差方程" 英文翻译 :    observationequation
• "程差方程" 英文翻译 :    eikonal equation
• "积差方程" 英文翻译 :    product moment equation
• "人差方程" 英文翻译 :    personal equation
• "时差方程" 英文翻译 :    moveout equation
• "视差方程" 英文翻译 :    parallax equation
• "误差方差" 英文翻译 :    error mean square; error variance
• "误差方向" 英文翻译 :    direction of error; error direction
• "约化残差方程" 英文翻译 :    reduced residual equation
• "区间误差方差" 英文翻译 :    between plot error variance
• "区均误差方差" 英文翻译 :    plot mean error variance
• "有效误差方差" 英文翻译 :    effective variance of error
• "误差方差；误差偏差" 英文翻译 :    error variance
• "误差方向, 失配方向" 英文翻译 :    direction of error
• "程差方程 程函方程 镜像方程 镜像方程" 英文翻译 :    eikonalequation
• "跟踪环相位误差方差" 英文翻译 :    tracking loop phase error variance
• "方程内误差" 英文翻译 :    error in equation
• "方程误差" 英文翻译 :    error in equation
• "方程误差模型" 英文翻译 :    error-in-equation model
• "交叉方程误差相关" 英文翻译 :    cross-equation error correlation

• In this paper , the od error equations are proposed in detail
  本文详细推导了里程计的速度误差方程。
• Depending on the error analysis of the strap - down inertial navigation system , the error equation of this system is given
  在分析捷联系统误差的基础上，给出了系统的误差方程。
• At the same time , we use kalman filter error equations in errors analysis for autonomous navigation algorithm , and compare the analysis results of the two methods
  同时利用卡尔曼滤波误差方程对自主导航算法进行误差分析,并将两种分析结果作比较。
• This paper utilizing the deduced error equation of apsse , establishing the equation be convenient to usign the monte carlo method , providing a new method to anglicizing the error of apsse
  论文利用推导出机载光电跟踪测量设备的位置传递方程基础上所建立的适合蒙特卡洛法的误差方程是对机载光电跟踪测量设备误差分析提供新的手段和方法。
• Initial alignment is to put on some speed of control angel in order to transferring the maths platform to expected location . it can be controlled by error equation . in the platform system , it used to adopt the modern control theory method
  初始对准从控制上讲就是施加一定的控制角速度把数学平台转向期望的位置(与地理坐标系重合) ，它是按误差方程进行控制的，过去在平台系统中采用频率特性方法，目前已经采用了现代控制理论设计方法。
• On the basis of kinematics analysis and model transformation , an error equation of the robot kinematics parameter is established with numerical optimization , and the optimal design for kinematics parameter is realized , which effectively increases the repositioning precision of the robot
  在运动学分析和模型变换的基础上，运用数值优化技术建立了机器人运动学参数的误差方程，实现了运动学参数的优化设计，有效提高了机器人的重复定位精度。
• The noise estimation theory of the gps / ins integrated navigation system and the error analysis is are systematically discussed in this dissertation . at first the paper briefly introduce the error of the integrated system and the cause of the error , and give an estimation model of the error . in order to solve the precise estimation of the error using artificial neural network , then an artificial neural network model is discussed
  本论文首先介绍了gps惯性组合导航系统的误差和误差模型，综述了gps和惯导系统的误差和误差来源，给出了这两种导航系统的误差方程，讨论了导航系统中常用的数据处理方法?卡尔曼滤波，给出卡尔曼滤波的基本方程，深入研究了卡尔曼滤波在组合导航系统数据融合中的应用。
• The paper presents the form of sins / odometer ( od ) / global position system ( gps ) integrated navigation system based on sins . state and observation equations are established for kalman filter . the simulation result shows that the integrated navigation system can reduce navigation error when using the feedback calibration method
  对捷联惯导系统、里程仪( od )和全球定位系统( gps )误差方程进行了分析，建立了以捷联惯导系统为主的用于卡尔曼滤波的系统方程和观测方程，给出了车载组合导航系统的分布式滤波组合方案。
• Two types of alignment algorithms on moving base were put forward in this paper , one with angular velocity matching , and another with acceleration matching . the error models and measurement models in consideration of ship flexure and lever - effect were deduced respectively . the alignment methods were verified by simulation
  提出了两种动基座传递对准的方法，一种是采用角速率匹配，一种是采用加速度匹配，并分别推导了在考虑船体变形和杆臂效应时传递对推的误差方程和量测方程，通过仿真验证了这两种传递对准方法的正确性。
• The improvements in the iaga contained adding strengthen operator , improving evaluation index of premature , etc . multi - phase homing project , making use of the flight properties of parafoil system in gliding and turning , was simple in control and facile in practice . based on frenet frame , the linear time - variable error equations of parafoil system were built
  基于frenet坐标系推导和建立了翼伞系统线性时不变的误差方程,并运用“投影点”的思想来获得frenet坐标系下偏差量的解析近似表达式,从而设计了用于翼伞系统航迹跟踪的传统pd控制器和增益调节型模糊pd控制器。