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navigation error中文是什么意思

  • 導(dǎo)航設(shè)施
  • 導(dǎo)航誤差

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  • Some teams may cover twice the distance due to their route and navigation errors
    有的隊(duì)由于路線及識(shí)圖越野出現(xiàn)偏差,可能要走兩倍于直線距離的路程。
  • And in the early time many integrated navigation error model was come into being . in all of them the model derivated by britting and widnall was the representative
    最具代表性的是利用britting和widnall推導(dǎo)出的誤差模型,該模型是基于地理系,考慮到系統(tǒng)誤差和傳感器誤差。
  • After the instrument error of sins is analyzed , it can be concluded that the quadratic model is more sensible to navigation error , and with instrument error taken into account , the linear model is better than the quadratic model
    通過(guò)捷聯(lián)慣導(dǎo)儀器誤差的分析,發(fā)現(xiàn)二次模型對(duì)捷聯(lián)慣導(dǎo)導(dǎo)航參數(shù)誤差更為敏感,考慮慣導(dǎo)儀器誤差后,線性模型的修正效果要優(yōu)于二次模型。
  • 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
    對(duì)捷聯(lián)慣導(dǎo)系統(tǒng)、里程儀( od )和全球定位系統(tǒng)( gps )誤差方程進(jìn)行了分析,建立了以捷聯(lián)慣導(dǎo)系統(tǒng)為主的用于卡爾曼濾波的系統(tǒng)方程和觀測(cè)方程,給出了車載組合導(dǎo)航系統(tǒng)的分布式濾波組合方案。
  • Abstract : the attitude error performance of electrostatic gyro should be understood and the relevant error equations must be set up in order to ensure the navigation precision of esgm . the relation between the navigation errors and the attitude errors of gyro was derived by use of spherical triangle . the simulation results show that the temporal performances of the longitudinal and distance errors which come from the initial alignment errors are periodically variational . they also show that the longitudinal and distance errors resulted from gyro drifts are not convergent in time . thus , the effects of initial alignment errors and gyro drifts can not be neglected and must be estimated and compensated
    文摘:為了保證靜電監(jiān)控器的導(dǎo)航定位精度,需要了解靜電陀螺的姿態(tài)誤差特性,建立相應(yīng)的誤差方程.本文采用球面三角形原理推導(dǎo)了導(dǎo)航定位誤差與陀螺姿態(tài)誤差的關(guān)系式.仿真結(jié)果表明,由初始定向誤差引起的經(jīng)度誤差和距離誤差的時(shí)間特性是周期變化的;由陀螺漂移引起的經(jīng)度誤差和距離誤差是隨時(shí)間發(fā)散的.因此,初始定向誤差和陀螺漂移的影響不能忽略,必須對(duì)其進(jìn)行估計(jì)和補(bǔ)償
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