捷聯慣導 的英文怎麼說

中文拼音 [jiéliánguàndǎo]
捷聯慣導 英文
sins
  • 捷 : Ⅰ形容詞（快; 迅速 ） prompt; nimble; quick Ⅱ名詞1. （勝利; 成功） victory; triumph 2. （姓氏） a surname
  • 聯 : Ⅰ動詞（聯結; 聯合） unite; join Ⅱ名詞（對聯） antithetical couplet
  • 慣 : Ⅰ動詞1 （習以為常 積久成性; 習慣） be used to; be in the habit of 2 （縱容; 放任） spoil; indulge...
  • 導 : 動詞1. （引導） lead; guide 2. （傳導） transmit; conduct 3. （開導） instruct; teach; give guidance to
  1. After the simulation of sins, the actual sins is studied, especially studying the compensation of gyro ' s excursion. and it proves that the compensation can improve the navigation accuracy of sins. on the basis of the realization of sins, the integrated navigation of position / velocity for gps and sins are established, and sins and gps integrated navigation is realized by application

    在實現sins的基礎上，研究了sins與gps的位置、速度組合導航，建立全球定位系統和捷聯慣導系統的誤差方程及位置速度測量方程，應用卡爾曼濾波技術實現了sins和gps的組合導航。
  2. Filtering algorithm of airborne gravimetry based on sins

    基於捷聯慣導的航空重力測量濾波演算法
  3. This paper regards a low cost piezoelectricity gyro sins and integration of it and gps as the target, make the research work of the following aspects

    本文以一個低成本壓電陀螺捷聯慣導系統及其與gps的組合為對象，做了以下幾方面的研究工作。
  4. The simulation results show that coning error and sculling error can be compensated satisfactorily in the algorithms. 3

    模擬結果表明：捷聯慣導演算法能實現對姿態圓錐誤差和速度劃船誤差的補償。
  5. The inertial sensors of the strapdown inertial navigation system ( sins ) are directly mounted to the vehicle and the vehicle ' s high - frequency motions will affect the accuracy of the sins

    捷聯慣導系統的慣性器件直接固聯在載體上，運載體的機動運動會直接影響系統的精度。
  6. The program are compiled in matlab language. the program include inertial device ideal simulation block > inertial device error simulator block, strapdown inertial navigation calculator block, doppler calculator block, kalman block and so on. the different block can be used for inertial navigation simulation, doppler simulation and so on

    用matlab語言編寫了水下航行器導航系統的模擬程序，這個程序包括：慣性器件輸出理想值模擬模塊、慣性器件誤差模擬模塊、捷聯慣導計算模塊、多普勒導航計算模塊、卡爾曼濾波模塊，可根據不同的需要進行純慣導狀態模擬、多普勒導航模擬、組合導航模擬。
  7. Application of coordinate transformations in the hardware - in - the - loop simulation of integrated navigation system

    航彈捷聯慣導系統半實物模擬試驗研究
  8. Calibration technique for shipboard missile sins

    艦載導彈用捷聯慣導系統校準技術研究
  9. The effect of range correction system of long - range rocket adopting sins is analyzed through numerical simulation

    通過數值模擬的方法，研究了採用捷聯慣導技術后遠程火箭射程修正效果。
  10. An independently integrated navigation system using odometer ( od ) to assist the strapdown inertial navigation system ( sins / od ) is discussed

    摘要利用里程計輔助捷聯慣導系統構成一種完全自主式的車載組合導航系統。
  11. Discusses an independently integrated navigation system ( sins ) using the distance - transfer - unit ( dtu ) to assist the strapdown inertial navigation system ( sins / dtu )

    摘要利用里程計輔助捷聯慣導系統構成一種自主式組合導航系統。
  12. 2. the updating algorithm of strapdown matrix is one of the crucial techniques of sins. there are several kinds of attitude updating algorithms of sins, such as direction cosine algorithm and quaternion algorithm

    捷聯矩陣更新演算法是捷聯系統的關鍵技術之一，捷聯慣導系統姿態演算法有歐拉角法、方向餘弦法、四元數法和圓錐補償演算法等幾種方法。
  13. Along with the improvement of rlg and accelerometer and the coming forth of high speed digital processor, the key technique of sins is carried out

    隨著激光陀螺和加速度計性能的不斷提高，以及高速數字處理器的不斷涌現，捷聯慣導系統實現的技術關鍵已經實現。
  14. The outputs of initial components have no errors. but many strapdown inertial navigation systems work in abominable environments, the outputs of the initial components include disturbance inevitably. as viewed from practicality, several algorithms were compared with each other, and it ' s shown that the forth order ronge - kutta is an algorithm suitable for practicality

    現有的捷聯航姿演算法均分析了純演算法誤差，即慣性元件的輸出為理想輸出，沒有任何誤差時的姿態誤差，然而許多捷聯慣導系統都工作在比較惡劣的環境中，慣性元件的輸出中不可避免地存在著干擾量。
  15. Compensation for the errors of the strapdown arithmetic in sins

    捷聯慣導系統的捷聯演算法誤差補償
  16. Because the data output of most of the inertial sensors in sins is in incremental form, the fundamental theory of sins based on the data output form is described in this thesis

    針對當前捷聯慣導系統中慣性器件的輸出大多採用增量形式的數據輸出，簡要介紹了適合於增量形式數據處理的捷聯演算法基本理論。
  17. Under the background of the strapdown integrated navigation system ( sins ), designs some sins with arinc 429 interface, analyzes the communication protocol, and in the guarantee of the system precision and the real - time request, accomplishes the modularized software of the arinc429 interface subsystem, and gives long time debugging and testing results to the sins system. this paper designs the airborne integrated navigation system based on the 1553b bus, completes the bus information flow design, and carries on thorough analysis on the communication protocol of the 1553b bus

    本文結合捷聯組合導航系統的應用背景，設計了含有arinc429總線介面的某型捷聯慣導系統，分析了其中的arinc429總線協議，並在保證系統精度和實時性的要求下，完成了該捷聯組合導航系統中arinc429介面系統的模塊化軟體設計，並給出對系統長時間聯調測試的分析結果。
  18. The rotation control technology in the laser gyro strapdown inertial navigation system was studied. the method of realizing closed - loop digital control with rlg located in the strapdown inertial navigation system was discussed. the structure of rotation servo system was introduced. the designing method and process of the digital controller were given. the method of implementing digital controllers by means of computer and software flow were demonstrated. the result of simulation and debugging of this system showed that it fullfills the requirment of the strapdown inertial navigation system. it assures the stability of rotation and solves the problem of striking without increasing the volume and cost of the system

    研究激光捷聯慣導系統中的轉位控制技術.採用捷聯慣導系統本身的rlg實現轉位系統的閉環數字控制，給出了轉位伺服系統的結構組成以及數字控制器的設計方法和設計過程，給出了數字控制器的計算機實現方法和軟體流程.模擬及調試結果表明，所設計的轉位伺服系統滿足捷聯慣導系統的要求，既保證了轉動的平穩性，克服了到位撞擊問題，又不增大體積、增加成本
  19. Adopt project practical quaternion algorithm of strapdown navigation system, analyze systematic error source, emulation prove the output change of sins in there is device error of inertia and the initial condition of collimation error

    採用了工程上實用的四元數捷聯導航系統的演算法，分析了系統誤差源，模擬驗證了捷聯慣導系統在有慣性器件誤差及初始對準誤差情況下的輸出變化。
  20. 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

    對捷聯慣導系統、里程儀（ od ）和全球定位系統（ gps ）誤差方程進行了分析，建立了以捷聯慣導系統為主的用於卡爾曼濾波的系統方程和觀測方程，給出了車載組合導航系統的分散式濾波組合方案。
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