進動陀螺儀 的英文怎麼說

中文拼音 [jìndòngtuóluó]
進動陀螺儀 英文
precession gyroscope
  • : 進構詞成分。
  • : 名詞[書面語]1. (山岡) low hill; hillock2. (團狀物) lump
  • : 1. [動物學] (軟體動物) spiral shell; snail; conch 2. (螺旋形的指紋) whorl (in fingerprint)
  • : 名詞1 (人的外表) appearance; bearing 2 (禮節; 儀式) ceremony; rite 3 (禮物)present; gift 4 ...
  • 陀螺儀 : gyroscope; gyro; top
  • 陀螺 : [物理學] top; whipping top; gyroscope; scopperil
  1. The key components in laser gyro is he - ne ring laser, and the reciprocal action theory between light and medium is the base in studying the ring laser, use the lamb half classical theory, and on the base of density matrix theory, the optical brounch equation was established, which described the movement of amplifying medium atom in the ring syntonic cavity, and according to the medium polarize theory the self consistent equations was deduced, which describe the light intensity and phasic of the counter - propagating wave. on the basis of this equations, adopted the simulation software matlab and virtual instrument programming language labwindows / cvi, we can do some simulated experiments in study the phenomenas such as amplify and dispersive characteristic of medium, mode pushing effection, burned hole effection and pattern competition, lock - in of frequency and the characteristic of light intensity and phasic of the counter - propagating wave in laser gyro

    激光的核心部件為he - ne環形激光器,而掌握光與介質的相互作用理論是研究激光器的關鍵,採用拉姆半經典理論為主,在密度矩陣理論的基礎上,推導環形諧振腔中描述he - ne氣體增益介質原子運的光學布洛赫方程,運用介質極化理論得出描述激光反向行波的光強、位相所滿足的自洽場方程組,在此基礎上,運用matlab模擬軟體和虛擬器編程語言labwindows / cvi ,對激光中的介質增益色散特性、頻率牽引效應、燒孔效應及模競爭、閉鎖效應及環激光的光強和相位特性行模擬試驗研究,並且運用全量子理論,對激光工作原理行分析,得出二能級系統單模輻射場的光子數密度分佈,得出激光場的光子統計分佈,模擬激光場的態建立過程。
  2. In the base of rigid body kinematics, the equations of attitude computation was developed via the imu sensor ’ s output, and a new method of the integrated attitude determination using gyroscope ’ s dynamic output and accelerometer ’ s static output was presented

    基於剛體運學,本文給出了由慣性測量單元的輸出所確定的氣浮臺姿態解算方程,並提出了利用態輸出與加速度計的靜態輸出行組合的姿態確定方法。
  3. The generalized coordinate of dtg with error in technics is studied. using, the dtg motion analysis is done

    研究了具有工藝偏差的力調諧速率的廣義坐標,利用廣義坐標對力調諧速率行了運分析。
  4. By researching and analyzing the system, it is known that the dynamic performance of the gyro bracket and isolation device is the key index of the dynamic performance in the system

    經對系統行研究分析得知,支架與隔振裝置的態性能是系統態性能的關鍵指標。
  5. On the base of the character of hemisphere continuously vibrating, the method of actuation and measuring, the asymmetry compensating process and the measuring limit were studied, the control loop and the parameter design were introduced, which will be prepared for the future circuit design and the automobile security application

    本論文主要是在半球連續振特性的基礎上,對的驅及感測方法、非軸對稱的補償方法及感測極限行研究,並詳細介紹其控制迴路與其參數的設計,為以後電路設計和面向汽車安全的應用打下了堅實的理論基礎。
  6. Fiber optic gyroscope ( fog ) is an advanced instrument to measure the angle velocity of rotation body. it realizes the measurement of optical sagnac effect using solid all - fiber structure. it overcomes mechanical - electrical gyro and ring laser gyro ' s reduction of dynamic performance and life - span caused by the structure or the requirement of high rotation rate mass

    光纖是一種先的感測載體自轉角速度的測量,它利用固態的全光纖結構實現光學sagnac效應的量測,克服了機電及環形激光在構造上或因需要一定的高速度旋轉質量,導致態性能及壽命的降低,或因諧振要求過于苛刻,使工藝復雜性及成本過高等一系列缺點,從而成為當今最具有競爭性的新型
  7. Fiber optic gyroscope ( fog ) is an advanced instrument to measure the angle velocity of rotation body. it realizes the measurement of optical sagnac effect using solid all - fiber structure. it overcomes mechanical - electrical gyro ' s reduction of dynamic performance and life - span caused by the structure or the requirement of high rotation rate mass, and the laser gyro ' s fabrication technology complication and high cost caused by the rigid requirement of optical circuit resonation

    光纖是一種先的測量載體絕對角速度的表,它利用固態的全光纖結構和sagnac效應來實現測量,克服了機電在構造上需要一定的高速度旋轉質量,導致態性能及壽命的降低,或者環形激光因諧振要求過于苛刻,使工藝復雜性及成本過高等一系列缺點,從而成為當今最具有競爭性的新型
  8. The research in the dissertation shows that the dtg with the larger angular velocity is not only with simple structure, but also its largest torquing rate can attain to 500 / s, it could fit the requirements of strap - down inertial navigation system completely. the dig with the larger angular velocity is a kind of mini inertial instrument that possessing of upper performance and is worthy to be studied ulteriorly

    本文的研究表明,大角速率調不僅結構簡單,而且最大施矩角速率可達500 s以上,可滿足捷聯慣導系統對測量范圍的要求,是一種值得一步研究的、具有較高性能的小型慣性表。
  9. Different filtering methods have been tested to examine the effects of all kinds of filters. the correction of inertial sensor errors, navigation algorithm, coning motion, and sculling motion have also been investigated. based on the above works, the initial alignment on stationary base using imu with mdrlg has been carried out, and an usable navigation software has been completed

    對機抖激光引起的高頻振的補償方法行了研究,對不同的濾波方法行了試驗;對機抖激光捷聯系統的表誤差補償、導航解算演算法、圓錐補償演算法和劃槳效應補償方法行了研究;對靜基座條件下機抖激光捷聯慣導系統的初始對準方法行了研究,編寫了實用的導航軟體。
  10. Positive tilting, real - time measurement and the compensation of gyroscope are the development trend of the tilting control system

    擺、在線實時數據採集和採用行補償是擺式列車傾擺控制系統的主流。
  11. This paper researched dynamic characteristics of internal and external bracket, the carrier of laser gyro, and compared kinds of scheme of structural design applying theory of structure dynamic design and theory of optimal design and analyzed natural characteristics of internal and external bracket applying ansys finite element analysis software. and use experimentation to validate this analysis result

    本文深入研究了激光的載體? ?內外支架結構的態特性,應用結構態設計理論及優化設計理論比較了各種設計方案,運用了有限元法分析了內外支架結構的強度和剛度,利用有限元力分析軟體ansys計算得到內外支架結構的固有頻率和振型,並通過試驗模態分析的方法行驗證。
  12. The algorithms " accuracy is compared with the traditional quaternion algorithm via digital simulations. the simulation results are accord to the theory conclusion. and in this paper, it is discussed that how to select the optimal sample algorithm and how to make full use of the gyro data per update

    在純錐運條件下行了數字模擬,對各演算法的精度行了比較,模擬結果與理論結果一致,另外對如何選取旋轉矢量幾階子樣演算法作為姿態更新演算法,以及如何合理利用輸出信息的問題行了說明; 5
  13. The kinematic model of inertial measurement unit ( imu ) with mdrlg has been analyzed theoretically, the coning drift caused by dithering has been calculated, and some problems including the assembly of inertial sensors have been discussed

    本文對機抖激光捷聯慣導系統慣性測量單元的運模型行了理論分析,對抖作用下的圓錐漂移行了理論計算,對表安裝形式等問題行了探討。
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