漂移误差的英文

• drift error
• wander error

• "漂移"英文翻译    be driven by the current; dr ...
• "误差"英文翻译    error
• "零点漂移误差" 英文翻译 :    zero drift error; zero-drift error
• "零位漂移误差" 英文翻译 :    zero drift error
• "漂移误差补偿" 英文翻译 :    drift error compensation
• "角位移误差" 英文翻译 :    angular travel error
• "偏移误差" 英文翻译 :    bias error; displacement error; drift error; offset error
• "位移误差" 英文翻译 :    di lacement error; displacement error; vector error
• "相位移误差" 英文翻译 :    phase angle error
• "冲击位移误差" 英文翻译 :    ballistic deflection error
• "地形偏移误差" 英文翻译 :    terrain distortion
• "指示位移误差" 英文翻译 :    indicated displacement error
• "航天飞船位移误差" 英文翻译 :    spaceship displacement error
• "漂移" 英文翻译 :    1.(漂流移动) be driven by the current; drift about2.[电子学] drift; shift; shifting; shunt running; creeping; wander◇漂移浮标 drifting buoy; 漂移度 driftance; 漂移晶体管 drift transistor; 漂移力 drift force; 漂移率 drift rate; drift mobility; 漂移区 drift region; 漂移速度 drift velocity; 漂移误差 drift error
• "误差" 英文翻译 :    error 平均误差 mean error; average error; 仪器误差 instrumental error; 概然误差 probable error; 行星观测上位置与计算上位置间的误差 the error of a planet; 误差极微的精密零件 precision parts with very close tolerances; 误差不超过千分之三毫米 with a tolerance of less than three-thousandths of a millimetre; 误差分析 error analysis; 误差概率 probability of error; 误差估计 error estimate; 误差函数 error function; 误差量 extent of error; 误差率 error rate
• "低漂移" 英文翻译 :    low drift
• "峰漂移" 英文翻译 :    peak shift
• "风漂移" 英文翻译 :    wind drift
• "氦漂移" 英文翻译 :    helium drift; heliumdrift
• "库漂移" 英文翻译 :    repertoire shift
• "零漂移" 英文翻译 :    zero drift; zero shift
• "慢漂移" 英文翻译 :    slow drift
• "漂移，偏航" 英文翻译 :    drift
• "漂移，移动" 英文翻译 :    wander
• "漂移；漂流" 英文翻译 :    float

• Zero - drift error
  零点漂移误差
• Mathematic expressions of static drift error and dynamic test error are formulated
  建立了陀螺静态漂移误差模型和动态漂移误差模型。
• The static drift error and dynamic test error of liquid floated reactive rate gyro are analyzed also
  分析了液浮力反馈速率陀螺的静态漂移误差和动态测量误差。
• Its static error is categorized into three types : irrelative with the specific force , relative with the first - order of specific force and relative with the square of specific force
  把漂移误差分为与比力无关、与一次方成比例和与二次方成比例三类。
• So the drift error of gyro is always the main source of error in the control and navigation system , the study of technology of measurement and compensation plays more and more important part in this field
  由于陀螺的漂移误差是整个控制和导航系统的重要误差源,所以,对陀螺仪漂移的测试及补偿技术的研究具有越来越重要的意义。
• Then two kinds of drift errors , which caused the decline of output video quality , were educed based on the theoretic analysis , and another kind of drift error , which was unique for transcoding in dct domain , was studied
  然后,根据理论分析,推导出了造成转码系统输出视频质量下降的两种漂移误差,并通过对不同结构转码系统仿真结果的比较,得出了dct域转码所特有的一种漂移误差。
• Performance for a piezoresistive transducer pressure sensor to thermal and pressure environments can be predicted by finite element method . a simplified 1 / 8 model , considering silicon dioxide and nitride process as well as stack anodic bonding and adhesive bonding processes , was developed . the fem results were found to be comparable to experimental data . case studies suggested that pyrex stack induces certain amount of non - linearity , while it isolates hard epoxy nonlinear effect . flexible epoxy bonding or soft adhesive bonding is preferred to the packaging process . the viscoelasticity and viscoplasticity of bonding material will result in hysteresis and drift errors to sensor output . however , soft adhesive s influence on sensor can be ignored under relative stable environments . more over , detailed design and process information will help to improve modeling application
  热、压环境下压阻变换压力传感器的性能可以通过有限元方法预测.这里研究了简化的1 / 8模型,模型考虑了二氧化硅和氮化硅生成过程及堆阳极键合和胶粘结合过程.结果发现有限元预测结果和实验数据具有可比性.范例研究表明,硼硅堆导致产生一定的非线性,但它隔离了硬环氧树脂的非线性.在包装过程中最好使用柔性环氧黏合或软黏胶性结合.黏合材料的黏弹性和黏塑性将会导致传感器输出的滞后和漂移误差.然而,在相对稳定的环境下,软黏合剂对传感器的影响可以忽略.此外,详细的设计和过程信息有助于提高模型的适用性
• Taking intercontinental ballistic missiles as objects under research , and based on the analysis of the influence of accelerometer measurement error and gyroscope excursion error on the apparent acceleration , the error transfer model of the inertial system in a midcourse guidance segment for velocity and location is given , and the pure inertial navigation guidance error is computed with the given imu error coefficient deviations
  摘要针对洲际弹道导弹，在分析加速度计测量误差和陀螺漂移误差对导弹视加速度影响的基础上，给出了中制导段惯性系统对速度和位置的误差传递模型，对给定的惯组误差系数偏差进行了纯惯性导航制导误差计算。

• 漂移误差的日语：ドリフトエラー