satellite attitude stabilization 中文意思是什麼

satellite attitude stabilization 解釋
衛星姿態穩定
  • satellite : n 1 【天文學】衛星;人造衛星;〈比喻〉衛星國。2 隨從,幫閑者,食客。3 【生物學】隨體(指染色體)...
  • 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。
  • stabilization : n. 穩定(作用),幣值的穩定;堅定,固定。 effect economic stabilization 實現經濟的穩定。n. -zator =stabilizer.
  1. Finally, attitude stabilization control of the satellite and pointing precision of the payload are researched in the phase of infrared camera tracking object

    第三,在紅外相機跟蹤目標階段,研究了星本體的姿態穩定控制以及有效載荷的指向精度問題。
  2. Through it the author made a deep study of the satellite attitude control subsystem, verified several sorts of disturbance torques and realized satellite three - axis attitude stabilization control and attitude maneuver under different conditions

    本文在simulink下對衛星姿控系統作了比較深入的研究,對各種干擾力矩進行了驗證,同時在不同的模擬條件下實現了衛星三軸穩定控制、姿態機動和飛輪的磁卸載。
  3. 4. the three - axis attitude stabilization system of the flexible satellite has been studied, in which three basic vibration modes of the solar array have been considered

    4 、在撓性衛星動力學模型的基礎上,建立了只考慮太陽帆板三階振動模態的撓性衛星三軸姿態控制模型。
  4. 3. the three - axis attitude stabilization of the rigid satellite has been studied. and, the influences of the external disturbances on the system stabilization have been studied

    3 、設計了剛體衛星的三軸姿態穩定控制律,分析了外界干擾對剛體衛星姿態的影響和系統的穩定性。
  5. The dynamic model of the satellite with a flexible appendage has been studied in this thesis. also, the techniques of the satellite earth acquisition and three - axis attitude stabilization of both the rigid satellite and the liquid - filled satellite have been researched

    本文針對單翼大撓性太陽帆板衛星,建立了撓性衛星動力學模型,在此基礎上,研究了地球捕獲、剛體衛星三軸姿態穩定、充液衛星三軸姿態穩定問題。
  6. Secondly, attitude stabilization control of the satellite is researched in the phase of infrared camera scanning object

    第二,在紅外相機掃描目標階段,研究了星本體的姿態穩定控制問題。
  7. Using quaternion as attitude representation, the attitude kinematics function is established. 2. several kinds of disturbance torques affecting the satellite attitude are directly computed through the models described in the paper, forming a closed loop stabilization system dumped by magnetic torques and provided with initial torques through flywheels, but other simulations only estimate it by experience

    ( 2 )很多模擬是根據經驗估算衛星所受的干擾力矩,本文以某對地觀測小衛星為背景,利用所建力學模型對衛星所受數種干擾力矩進行計算,形成了一個以飛輪作為主動力矩、通過磁力矩卸載的閉環而且穩定的姿態控制系統。
  8. Next, the characteristics of the user satellites complex control system is that the high accuracy antenna pointing control is realized on the basis of ensuring the high accuracy attitude stabilization control of the satellite body

    3 .用戶星復合控制系統的特點是在保證衛星平臺高精度姿態穩定控制的前提下,實現星間鏈路天線的高精度指向控制。
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