errors equation造句
例句與造句
- In this paper , the od error equations are proposed in detail
本文詳細(xì)推導(dǎo)了里程計(jì)的速度誤差方程。 - Depending on the error analysis of the strap - down inertial navigation system , the error equation of this system is given
在分析捷聯(lián)系統(tǒng)誤差的基礎(chǔ)上，給出了系統(tǒng)的誤差方程。 - 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
同時(shí)利用卡爾曼濾波誤差方程對(duì)自主導(dǎo)航算法進(jìn)行誤差分析,并將兩種分析結(jié)果作比較。 - This paper employs differentiation transformation and the method of differentiating completely homogeneous coordinate transformation to set up errors equations group , the discussion of the errors of double - triangle pkm is conducted
本論文應(yīng)用微分變換和齊次坐標(biāo)變換的全微分建立誤差方程組，討論了雙三角形并聯(lián)機(jī)構(gòu)的位姿誤差分布。 - 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
論文利用推導(dǎo)出機(jī)載光電跟蹤測(cè)量設(shè)備的位置傳遞方程基礎(chǔ)上所建立的適合蒙特卡洛法的誤差方程是對(duì)機(jī)載光電跟蹤測(cè)量設(shè)備誤差分析提供新的手段和方法。 - It's difficult to find errors equation in a sentence. 用errors equation造句挺難的
- Based on the error distributing of the apsse , we established the error equation helped to calculate the error of appse usign the matlab software . then we designed and wrote the emulating program of the apsse measuring equation
論文在機(jī)載光電跟蹤測(cè)量系統(tǒng)的位置傳遞方程的基礎(chǔ)上，利用matlab程序的特點(diǎn)，編寫了機(jī)載光< wp = 5 >電跟蹤測(cè)量系統(tǒng)的測(cè)量方程仿真計(jì)算程序。 - Since there are over twenty taches from the object to the photo , the error analysis method is firstly unit analysis and the synthesize . after established the error equation usign the coordinate transform method , quantificational anglicizing the total error is possible
建立位置傳遞方程的目的就是將這些誤差用方程的形式統(tǒng)一起來，改變以往對(duì)誤差的分析都是先進(jìn)行單元分析，然后，進(jìn)行合成的缺陷。 - 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
初始對(duì)準(zhǔn)從控制上講就是施加一定的控制角速度把數(shù)學(xué)平臺(tái)轉(zhuǎn)向期望的位置(與地理坐標(biāo)系重合) ，它是按誤差方程進(jìn)行控制的，過去在平臺(tái)系統(tǒng)中采用頻率特性方法，目前已經(jīng)采用了現(xiàn)代控制理論設(shè)計(jì)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
在運(yùn)動(dòng)學(xué)分析和模型變換的基礎(chǔ)上，運(yùn)用數(shù)值優(yōu)化技術(shù)建立了機(jī)器人運(yùn)動(dòng)學(xué)參數(shù)的誤差方程，實(shí)現(xiàn)了運(yùn)動(dòng)學(xué)參數(shù)的優(yōu)化設(shè)計(jì)，有效提高了機(jī)器人的重復(fù)定位精度。 - We have known from the analysis of error equations of sins that the errors produced by the initial alignment will propagate with time , the precision of initial alignment will affect the precision of the whole system , and so it is very important to improve the precision of initial alignment
從捷聯(lián)慣性系統(tǒng)誤差方程的分析可知，初始對(duì)準(zhǔn)誤差會(huì)隨時(shí)間而傳播，初始對(duì)準(zhǔn)的精度直接影響整個(gè)捷聯(lián)系統(tǒng)的系統(tǒng)精度，因此提高初始對(duì)準(zhǔn)的精度對(duì)改善捷聯(lián)系統(tǒng)精度是至關(guān)重要的。 - In this paper , the main navigation methods and the principle of sins navigation are introduced . according to the principle of sins , it calculates and simulates the observations of sins through prearranged track , deduces the error equations of initializing alignment of sins , simulates the process of alignment
本文首先介紹了當(dāng)前各種導(dǎo)航手段和方法，論述了捷聯(lián)慣性導(dǎo)航系統(tǒng)( sins )的導(dǎo)航原理，針對(duì)艦船運(yùn)動(dòng)的特點(diǎn)，對(duì)sins的導(dǎo)航工作過程，進(jìn)行了仿真計(jì)算。 - This paper stated the application of parallel link mechanism in modern machine tools , set up the error analysis as to parallel link mechanism in the virtucal - axis machine tool , derived the double triangular error equations of parallel link mechanicsm in its horizontal posture , analyzed the linearity and non - singularity of the error equations , thus giving the normal splution to the horizontal posture error . the error distribution law is simulated as to the center line in the workplace , and the error distribution curves are drawn as well
該文對(duì)并聯(lián)機(jī)構(gòu)在現(xiàn)代機(jī)床上的應(yīng)用作了論述，建立了虛擬軸機(jī)床并聯(lián)機(jī)構(gòu)的一種誤差分析方法，應(yīng)用坐標(biāo)變換原理導(dǎo)出了雙三角并聯(lián)機(jī)構(gòu)水平姿態(tài)時(shí)的誤差方程組；分析了誤差方程組的線性和非奇異性，給出了水平姿態(tài)時(shí)的位姿誤差正解；對(duì)工作空間中心線的誤差分布規(guī)律進(jìn)行了仿真，繪制了其誤差分布曲線。 - Its brings forward data processing means , discusses estimate means and spread rule of random error and system error , presents error equation , validates adequately by theory analysis combining practice , obtains a great deal experiment data , finds change rule of vehicle plane error
提出了數(shù)據(jù)處理的方法，討論了隨機(jī)誤差和系統(tǒng)誤差的估計(jì)方法和傳播規(guī)律，給出各單項(xiàng)誤差的方程，把理論分析與實(shí)踐相互結(jié)合，進(jìn)行充分驗(yàn)證，獲得大量實(shí)驗(yàn)數(shù)據(jù)，得到車載平臺(tái)誤差的變化規(guī)律，通過仿真驗(yàn)證了數(shù)學(xué)模型的正確性。 - 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
本文首先研究了車載捷聯(lián)慣導(dǎo)系統(tǒng)( ins )的零速修正技術(shù)，在分析捷聯(lián)慣導(dǎo)系統(tǒng)誤差方程特點(diǎn)的基礎(chǔ)上，推導(dǎo)了停車時(shí)利用ins速度輸出估計(jì)姿態(tài)誤差角的方法，并對(duì)用二次曲線擬合姿態(tài)誤差角的兩種方案作了比較，提出了按時(shí)間分段確定擬合系數(shù)的方法。 - 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坐標(biāo)系推導(dǎo)和建立了翼傘系統(tǒng)線性時(shí)不變的誤差方程,并運(yùn)用“投影點(diǎn)”的思想來獲得frenet坐標(biāo)系下偏差量的解析近似表達(dá)式,從而設(shè)計(jì)了用于翼傘系統(tǒng)航跡跟蹤的傳統(tǒng)pd控制器和增益調(diào)節(jié)型模糊pd控制器。
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