attitude angular velocity 中文意思是什麼

attitude angular velocity 解釋
姿態角速度
  • attitude : n. 1. 姿勢,身段。2. 態度,看法。3. 【軍事】飛行姿態。4. 芭蕾舞的一個姿勢。
  • angular : adj. 1. 有角的,角形的;尖銳的。2. 用角度量的;角的。3. 瘦骨嶙峋的。4. 不靈活的,生硬的。adv. -ly
  • velocity : n. 1. 迅速;快速。2. 速度,速率。3. 周轉率。
  1. In addition, a series of reasonable time histories of helicopter velocity, angular velocity and flight attitude were shown during the given dolphin maneuver flight

    最後以黑鷹直升機為例計算了魚躍越障機動飛行時駕駛員操縱輸入及直升機速度、角速度和飛行姿態的變化規律。
  2. To solve the problems caused by the varieties of the missile dynamics with the difference of flight height, velocity and attitude angle in modeling the missile, in this thesis, the theory of variable structure model reference adaptive control is used to design a pitch channel autopilot based on a longitudinal missile model, the status equation using the measurable parameters of load and angular rate is established, and the methodology to choosing the reference model is discussed also, and the performance of the controller is analyzed by means of simulation

    為了解決攔截彈氣動參數隨飛行高度、速度、姿態的不同,變化范圍大,控制系統難以準確建模的困難,基於縱向平面攔截彈模型,採用模型參考變結構控制理論設計了俯仰通道姿控復合控制系統,以可測量變量過載和角速度作為狀態量建立了系統的狀態方程,討論了參考模型的選擇方法,並對系統的性能作了模擬分析。
  3. 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陀螺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;再利用光纖陀螺輸出的角速率信號,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位置。
  4. The attitude updating algorithms were investigated systematically in this paper. on the basis of the quaternion algorithm the coning compensation algorithms and the improved coning compensation algorithms the attitude updating algorithms were deduced when the gyro outputs are angular velocity. existing updating algorithms analyzed the accuracy of the algorithm, i. e

    本文對捷聯慣性導航系統捷聯矩陣的更新演算法進行了系統的研究,詳細地分析了四元數法、圓錐補償演算法、及在此基礎上發展起來的利用前一時刻陀螺儀輸出的改進圓錐補償演算法。
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