陀螺運動的英文怎麼說

中文拼音 [tuóluóyùndòng]
陀螺運動英文
circumgyrate

  • : 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)
  • : Ⅰ動詞1 (物體位置不斷變化) move; revolve 2 (搬運; 運輸) carry; transport 3 (運用) use; wield...
  • 陀螺: [物理學] top; whipping top; gyroscope; scopperil
  • 運動: 運動[舊時用語] arrange things or get things done through pull

※中文詞彙陀螺運動在字典百科國語字典中的解釋。

  1. A gyrocompass is required to indicate the heading of a land, sea, or air vehicle.

    被用來指示陸上的、海上的或空中的體的方向。
  2. Another test, involving the precession of a gyroscope in a satellite circling the earth, is scheduled for the 1970s.

    七十年代還安排了另一實驗,它包括繞地球旋轉的衛星中的性試驗。
  3. This gyroscopic motion is called precession.

    陀螺運動叫做進
  4. 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氣體增益介質原子的光學布洛赫方程,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,用matlab模擬軟體和虛擬儀器編程語言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進行模擬試驗研究,並且用全量子理論,對激光工作原理進行分析,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。
  5. Moment gyroscope is implement institution of the satellite attitude control system. the dynamics equation of single gimbal control moment gyroscope is set up, the control law of moment gycroscope is designed and the distribute matrix is confirmed reasonly

    選擇力矩作為該衛星控制系統的執行機構,建立單框力矩力學方程,在此基礎上進行力矩控制律設計,合理地確定力矩的分配矩陣。
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