位置陀螺 的英文怎麼說

中文拼音 [wèizhìtuóluó]
位置陀螺 英文
position gyro
  • : Ⅰ名詞1 (所在或所佔的地方) place; location 2 (職位; 地位) position; post; status 3 (特指皇帝...
  • : 動詞1. (擱; 放) place; put; lay 2. (設立; 布置) set up; establish; arrange; fix up 3. (購置) buy; purchase
  • : 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)
  • 陀螺 : [物理學] top; whipping top; gyroscope; scopperil
  1. The input axis of the azimuth gyro under this condition is vertical, and pendulum unit is nulled.

    在這樣情況下方的輸入軸是處於垂直,同時擺錘單元在零
  2. From the standpoint of the gyrocompass the earth appears to be rotating about an axis making an angle ε with the true polar axis.

    羅盤的觀察地球,好象地球是繞著偏離其極軸角的一個軸在移動。
  3. < uk > from the standpoint of the gyrocompass the earth appears to be rotating about an axis making an angle with the true polar axis. < / uk >

    < uk >從羅盤的觀察地球,好象地球是繞著偏離其極軸角的一個軸在移動。 < / uk >
  4. The gyro vertical utilizes a gyroscope as an integrating device to obtain the average position of a pendulous gravity reference.

    垂直利用一個儀作為積分裝以得搖擺不定的重力基準線的平均
  5. At first, according to the concrete requirement of the servo control system, a collective scheme, which provide guarantee to meet the requirements of the global performance, is established. in this scheme, the structure of gimbal and the torque motor driven mode are adopted, and angle measurement is accomplished by inductosyn and velocity measurement is accomplished by dynamically tuned gyro respectively

    首先,根據目標真值測量設備伺服系統的具體要求,確定了地平式常平架結構,力矩電機驅動,分別採用動力調諧式速率儀及圓盤式感應同步器作為速率及反饋元件這一總體方案,為伺服系統滿足整體性能指標要求提供了保證。
  6. The signal generator null sensitivity affects the accuracy and resolution of measurement because the gyro is an integrating device.

    因為是一種積分裝,所以信號發生器的零靈敏度影響測量精度和測量分辨度。
  7. The influence factors and optimal scheme of connected - triangle surveying with shaft is analyzed in detail. the formula for calculating the lateral transfixion errors of underground traverse with added gyro orientation line is derived strictly, the calculation results show that the accuracy can be increased obviously by the way of orienting added gyro lines

    詳細分析了聯系測量各因素對方傳遞的影響,探討並比較了加測角后地下導線的精度提高問題,論證了加測角后直伸等邊導線終點精度的嚴密計算公式及邊布測的最佳
  8. Based on analysis of the iso - rigidity of the gyro assembly, the requirement for making the joints match each other is offered, which has a guiding significance for joints assembly and selection. based on analysis of rigidity and drift error for the dynamically tuned gyro, a cross model including an inner and an outer flexible hinges is established

    在對動力調諧剛度和漂移誤差分析的基礎上,建立了由內外撓性接頭裝配所形成的十字型鉸鏈模型,並利用偽剛度理論對該模型進行了分析,得出了內外撓性接頭兩鉸鏈的相對關系對十字型鉸鏈模型的影響曲線。
  9. Taking intercontinental ballistic missiles as objects under research, and based on the analysis of the influence of accelerometer measurement error and gyroscope excursion error on the apparent acceleration, the error transfer model of the inertial system in a midcourse guidance segment for velocity and location is given, and the pure inertial navigation guidance error is computed with the given imu error coefficient deviations

    摘要針對洲際彈道導彈,在分析加速度計測量誤差和漂移誤差對導彈視加速度影響的基礎上,給出了中制導段慣性系統對速度和的誤差傳遞模型,對給定的慣組誤差系數偏差進行了純慣性導航制導誤差計算。
  10. The desired output information was a measure of slew-rate or angular-velocity input and not position.

    所要求的輸出是旋轉速率或角速度輸入的量度,而不是的量度。
  11. In this system, the closed loop is composed of velocity measurement machine used as velocity feedback and coder used as position feedback, the feed - forward signal of ship swaying is measured by rate gyro

    該系統用測速機構成閉環,作速度反饋,編碼器作反饋,速率測量並前饋艦船搖速度信號。
  12. As vital integral part of the laser gyro navigation system design, the study in the paper solved technical problems such as outcome distortion or even system failure resulted from bad dynamic performance of bracket and isolation device structure

    通過本文的研究,成功解決了激光儀定系統工作中,因支架與隔振裝結構動態性能差而出現的結果失真及至死機的技術問題。
  13. The first is dead reckoning, which computes its own positions from the direction and speed data continuously obtained from the gyroscope and speedometer in the vehicle

    第一是推測領航,指不斷由車輛的儀和速度計顯示的方向和速度數據計算本身的
  14. On the aspect of errors analysis of hrg, a brief introduction of the close - loop detection theory of hrg is present first. later the expressions of close - loop detection errors are deduced in theory. the impact of stimulating signals, turning speed, outside appended oscillation, the location & area of electrodes, and the current loss in capacitor is considered, and the primary analysis of error compensation is given

    在半球諧振誤差分析方面,本文從半球諧振的閉環檢測原理出發,對半球諧振閉環檢測誤差進行了分析和推導,考慮了激勵信號、轉動速率、外界附加振蕩、電極及極板面積和電容傳感器等因素造成的誤差並對誤差補償進行初步分析。
  15. Fiber optic gyro ( fog ) inertial system provides angular velocity and acceleration measurement of measurement body along three axes, based on the attitude matrix refreshed by outputs angular velocity to transform the acceleration from the body frame to the earth frame, finally through acceleration integral we can get the position of the measurement body in the space. fog is popular in the navigation field for many advantages, such as wide dynamic range, high resolution and all solid components

    該測量方法利用捷聯式光纖輸出的角速度和加速度信息,測出運載體沿三個方向的加速度分量;再利用光纖輸出的角速率信號,不斷更新測量體的姿態轉換矩陣,將加速度分量用轉換矩陣更換到地理坐標系;最後經過計算機對轉換后的加速度信號積分運算分別可得到運載體在三維空間中的
  16. The results indicate that : with sa, the position precision of the integrated system, whose gyro drifting is 50 degree / hour and whose accelerator offset is 0. 001g, is 60 meters, its velocity precision is about 1. 75m / s out and its attitude angle precision is about 0. 25 degree. without sa, the position precision is about 20 meters, its velocity precision is about 0. 5m / s and its attitude angle precision is about 0. 1 degree. when the signal of gps is lost, the growing rate of the integrated system error is much lower than that of sins system

    模擬結果表明:對于漂移為50度/小時、加速度計零偏為0 . 001g的組合系統,在有sa的情況下,精度大約為60米,速度精度大約為1 . 75米/秒,姿態角精度大約為0 . 25度;在無sa的情況下,精度大約為20米,速度精度大約為0 . 5米/秒,姿態角精度大約為0 . 1度;在gps信號丟失時,系統誤差的增長速度比純sins系統明顯減緩。
  17. In the latter, that is in two - position alignment, the method of wavelet analysis is used to filter the output signal of optic fiber optic gyro, at last, the direction cosine matrix is gotten, the inertial components are demarcated,

    在自對準中,利用二初始對準,運用小波分析對光纖的輸出信號進行濾波,並且確定初始方向餘弦矩陣並對慣性元件進行標定。
  18. Using gyro measurements during periods of thruster firing, with thruster outputs, mass property identification is achieved through recursive least squares algorithms on the basis of the refined dynamics equation. the approach addresses the issue by segmenting the problem into two sub - problems which both allow closed form solution to reduce computation load

    該方法利用衛星上的輸出和推力器控制指令作為演算法的輸入,在修正的衛星姿態動力學模型基礎上,推導了衛星質量特性在線辨識遞推最小二乘演算法,將質心和轉動慣量矩陣的辨識解耦以降低辨識演算法的維數,減少計算量。
  19. When a position gyro is used in the pitch plane the missile is usually launched at a set elevation.

    位置陀螺用在俯仰平面上的時候,導彈通常以一個設定的仰角發射。
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