捷聯慣導系統,SINS英語短句,例句大全

捷聯慣導系統,SINS
1)SINS[英][sin][美][s?n]捷聯慣導系統
1.A Fast Method for SINS Initial Alignment of AUV on a Locomotive Base;一種AUV捷聯慣導系統動基座快速初始對準方法
2.Formation mechanism for static conning motion of mechanically dithered ring laser gyro SINS;機抖激光捷聯慣導系統靜態圓錐運動形成機理
3.Swing Error Compensation in Coarse Alignment for Land SINS;車載捷聯慣導系統粗對準中擺動誤差補償研究

英文短句/例句

1.Research of SINS Initial Alignment on Dynamic Base捷聯慣導系統晃動基座初始對準研究
2.Optimal Design for Sculling algorithms of SINS捷聯慣導系統劃船效應補償算法研究
3.The Research of Hardware of Strapdown Inertial Navigation System Based on FOG;光纖陀螺捷聯慣導系統硬件電路研究
4.The Research of Filter Technic in Inertial Alignment of Strapdown System;捷聯慣導系統初始對準濾波技術研究
5.The Research and Design of Initial Alignment in Strapdown Inertial Navigation System;捷聯慣導系統的初始對準研究與設計
6.The Low Cost Inertial Navigation System Based on MEMS基于MEMS的低成本捷聯慣導系統實現
7.The Study on Temperature Effect Compensation for Fiber-optic Strapdown Inertial Navigation System光纖捷聯慣導系統溫度效應補償研究
8.A Practical Algorithm for Speed Error Compensation of SINS捷聯慣導系統速度誤差補償實用算法
9.Rapid Design of Strapdown Inertial Navigation System Based on Matlab/Simulink基于Matlab/Simulink捷聯慣導系統快速設計
10.Technique of continuous auto-calibration of redundant strapdown inertial system余度捷聯慣導系統連續自動標定技術
11.Research on rapid transfer alignment for the airborne missiles SINS機載導彈捷聯慣導系統快速傳遞對準方法研究
12.Researches on the Strapdown Inertial Navigation System Algorithms in the Frequency and Wavelet Domain;捷聯慣導系統頻域與小波域內導航算法研究
13.Integrated navigation method of strapdown inertial navigation system under damping condition阻尼狀態下捷聯慣導系統組合導航方法探討
14.Digital Simulation Study of SINS of a Small Tactical Missile小型戰術導彈捷聯慣導系統數字仿真研究
15.Measurement Error Model of IMU in Strapdown Inertial Guidance System of Manpads Missile單兵導彈捷聯慣導系統IMU測量誤差模型
16.strap-down inertial navigation system捷聯式慣性導航系統
17.Study on High-accuracy Algorithms in the SINS;高精度捷聯式慣性導航系統算法研究
18.Study of Alignment Techniques on the Strap-down Inertial Navigation System;捷聯慣性導航系統初始對準技術研究

相關短句/例句

Strapdown inertial navigation system捷聯慣導系統
1.New coning error compensation algorithm of strapdown inertial navigation system;一種新的捷聯慣導系統圓錐誤差補償算法
2.Error characteristic analysis of strapdown inertial navigation system;捷聯慣導系統誤差特點分析
3.The Research of Key Technique of FOG Strapdown Inertial Navigation System Based on DSP;基于DSP的光纖陀螺捷聯慣導系統關鍵技術研究
3)strapdown inertial navigation system(SINS)捷聯慣導系統
1.By analysing systematically from theoretical point of viewing the installation error in strapdown inertial navigation system(SINS),the system s error model when there are both position-installing error and angle-installing error is concluded,and the influence on SINS s accuracy caused by installation error is simulat.針對捷聯慣導系統(SINS)中的機載安裝誤差進行了深入全面的研究,推導出角安裝誤差和位置安裝誤差同時存在時系統的誤差模型,并對機載安裝誤差給導航系統精度帶來的影響進行了系統仿真。
2.Based on the characteristics of shipbased weapons,an error model of strapdown inertial navigation system(SINS) is established on a swaying base,and an autonomous initial alignment method of shipbased weapons is analyzed in details.基于艦載武器特點,建立了捷聯慣導系統(SINS)在搖擺基座下的誤差模型,詳細分析了一種艦載武器的自主式初始對準方案,在傳統反求桿臂長度補償桿臂效應方法的基礎上,提出了一種新的補償桿臂效應的方法,并通過仿真驗證表明,該方法比傳統的桿臂長度補償法具有更高的精度,研究結果可為艦載武器對準方案的選擇與設計提供理論依據。
3.Based on the fact that it is very difficult to improve the autonomous alignment accuracy of strapdown inertial navigation system(SINS),an error function for static-state initial alignment of SINS is built.針對目前提高捷聯慣導系統自對準精度難度大這一情況,在建立SINS靜基座初始對準的誤差方程的基礎上,通過對影響對準精度的誤差因素進行分析,提出了一種在載體內部安裝高精度自主尋北裝置的方法,該方法可有效地提高初始對準精度。
4)strap-down inertial navigation system捷聯慣導系統
1.Based on that,the emulation result for the software MATLAB was produced in the strap-down inertial navigation system.在此基礎上給出了對捷聯慣導系統的MATLAB軟件仿真結果,仿真結果表明,等效旋轉矢量算法可以實現對不可交換誤差的有效補償,算法關系簡單,易于操作,特別適用于角機動頻繁激烈或存在嚴重角振動的運載體的姿態更新。
2.A revising method is proposed,in which the velocity of Doppler velocity log(DVL) is used to aid the alignment of strap-down inertial navigation system with DVL and the integrated navigation based Kalman filter.提出了利用多普勒測速儀輔助捷聯慣導系統動基座對準以及基于卡爾曼濾波的組合導航方案,并對該導航方案水上實驗的結果進行了分析。
3.The design of high-precision fault-tolerant integrated navigation system (HINS) based on strap-down inertial navigation system (SINS) needs to consider a series of key technologies, such as high-precision SINS algorithms, information fusion, fault tolerant design and so on.針對當前捷聯慣導系統中慣性器件的輸出大多采用增量形式的數據輸出，簡要介紹了適合于增量形式數據處理的捷聯算法基本理論。
5)strapdown INS捷聯慣導系統
1.Application of Kalman Filter in Initial Alignment of Strapdown INS;卡爾曼濾波在捷聯慣導系統初始對準中的應用
2.To improve the attitude matrix and real time calculation of Strapdown INS,this paper introduces introduces three order resusive Taylor expandeded form of quaternion to updating attitude algorithm,especially discussing the method of simulation study and programming the corresponding simulatioin programs with C language to a land vehicle strapdown INS.為改進捷聯慣導系統姿態矩陣的解算、實時計算等問題 ,本文引入四元數三階泰勒展開遞推式作為捷聯慣導系統的姿態更新算法 ,著重解決了使用三階泰勒展開遞推式進行姿態計算的方法 ,并對某陸地捷聯慣導系統的量測數據 ,用 C語言進行了相應的仿真。
3.Aimed at calculating the attitude matrix of strapdown INS fast and preciously in the high maneuver condition,some current update methods of quaternion which always had been used was analyzed in the principle and calculating effect,besides,a new method was proposed in the proving process.針對在大機動條件下進行快速準確的捷聯慣導系統姿態矩陣解算,從原理上和計算效果上分析了現在較為常用的幾種四元數更新方法,并在推證的過程中使用了一種新的方式;該方法以三階泰勒展開為基礎,直接利用角速度的各階導數進行四元數的更新運算,最后準確地得出各個姿態角的值;通過對幾種仿真結果進行的具體分析,表明該方法在不增加采樣值的情況下,其計算的精度和計算時間都達到了其他算法在同等條件下無法達到的效果,可以有效的運用于大機動飛行條件下。
6)strapdown inertial navigation system(SINS)捷聯慣導系統(SINS)