共變坐標 的英文怎麼說

中文拼音 [gòngbiànzuòbiāo]
共變坐標 英文
covariant coordinates
  • : 共動詞[書面語]1. (圍繞) surround2. (兩手合圍) span with the hand
  • : Ⅰ名詞1 [書面語] (樹梢) treetop; the tip of a tree2 (枝節或表面) symptom; outside appearance; ...
  1. 2. dynamics analysis : by setting up jacon matrix differential coefficient sport is passed to descartes space. it makes terminal executing manipulator produce differential coefficient of acceleration and force in every different coordinates can be got. then the effective inertia, coincident inertia and gravity load of two manipulators are calculated by lagrange method. so generalized joint torque of each joint is got, and along with equivalent driving torque, actual driving torque of each joint can be worked out. 3

    動力學分析:建立雅可比矩陣將關節空間的各關節的微分運動傳遞到笛卡爾空間,使末端執行器位姿產生微分運動,以用於求加速度及力在不同系間的線性換,再用拉格朗日法計算兩機械手的有效慣量、偶合慣量、重力載荷,從而計算得到各關節的廣義關節力矩,並與等效驅動力矩同算得各關節的驅動力矩。
  2. At first the paper begin to study the foundation of digital curved face and space meshing principle, introduce the basic knowledge of curve theory and curved face theory, explain the mathematical tools of vector turning and coordinate conversion in the paper ; analyse the motion and relative motion of rigid body, provide the condition of gear driving continuous contact and equation of conjugate meshing

    論文首先從參數化曲面和空間嚙合原理基礎出發,介紹了曲線論和曲面論的基本知識,對課題研究重的數學工具矢量回轉和換進行了說明;分析了剛體的運動和相對運動,根據空間嚙合原理給出了輪齒傳動連續接觸的條件和軛條件方程。
  3. The conformal microstrip antenna with some unique character has been applied in many fields, especialy on speedy objects. in this paper, an efficient fdtd algorithm is introduced to analyse the microstrip antenna. firstly, the fdtd formula in descartes coordinate system and in cylindrical coordinate system are obtained from the time _ dependent maxwell equations using the yee algorithm in a calculating region where the dielectric parameters are independent of time and space. the choice of the space discretization units and the time discretization interval are discussed which are decided by the accuracy and stability respectively. the shape and setup of the excitation source are discussed too. the excitation source is chosen to be gaussian pulse in shape. secondly, the mur ' s first - order and second - order boundary condition are deduced in cylindrical coordinate system. the methods of transforming radiation fields from near zone to far zone in the frequency domain and in the time domain are presented when fdtd is applied to analyse the characteristics of far zone. finally, three kinds of microstrip antennas are analysed. they are a slot antenna that lies on a plane ground of a microstrip, a slot antenna that lies on a cylindrical ground of a microstrip and a microstrip line _ fed aperture coupled stacked rectangular patch antenna in cylindrical coordinate system

    本文從麥克斯韋旋度方程出發,建立了笛卡兒下無源空間中均勻無耗媒質的fdtd基本方程和圓柱下無源空間中均勻無耗媒質的fdtd基本方程,詳細討論了fdtd法計算中時間步長和空間步長的選取原則以及激勵源的類型和設置;推導了mur一階和二階邊界條件在圓柱下的差分格式;給出了在用fdtd法計算天線的遠場輻射特性時必需採用的頻域和時域近場遠場換技術;最後用fdtd法計算了平面微帶縫隙天線、柱面形微帶縫隙天線和柱面形微帶層疊天線的輸入阻抗和遠區輻射場,並分析了天線的一些參數的化對天線輸入阻抗的影響,得出了一些有用的結論。
  4. First, by using coordinate rotation, we have discussed the computer - generated hologram composed by planar object whose plane does n ' t run parallel with that of its hologram. second, through coordinate transform, the computer - generated hologram of curvy planar object has been discussed again, in which, conformal map in computer graphics has been creatively applied, and generated the computer - generated hologram of simple curvy plane ( e. g. spherical surface ) ; also, in this section, the correctness of transformation has been confirmed by numerical reconstruction

    首先利用旋轉討論不平行於全息面的平面所構成的物體的計算全息圖:接著採用換討論曲面物體的計算全息圖,創造性地將計算機圖形學中的形對應原理運用到計算全息中,生成了簡單曲面(如球面)物體的計算全息圖,並用數字重現驗證了換的正確性,為今後復雜三維物體的計算全息圖的研究奠定基礎。
  5. The effective optimization design programs for different cases are developed by integrating the following several aspects which involves the flow analysis, adjoint equation solution, gradient solution, optimal arithmetic and grid generation. some practical design tests for airfoil and wing show that the continuous adjoint approach is very effective and useful method for aerodynamic optimization design. at the same time, we have done the research of aerodynamic optimum design for airfoils by using navier - stokes equations

    ( 4 )研究了基於控制理論和三維navier一stokes方程的優化設計理論,在計算下詳細推導了該優化設計理論,得到了計算系下描述的扼方程數學描述形式,並以給定目壓力分佈的氣動反設計為例,導出了相應的扼方程邊界條件,以及關鍵的梯度求解具體表達形式,為了求解方便,把計算空間上描述扼方程表達形式換到物理空間中進行描述,通過與ns方程表達形式對比分析,最終給出了一種直觀的轆方程表達方式。
  6. The information along 3d maximum shear stress tracing line is completely ascertained with the method of parameter transformation, then the changing rule of the normal stress along 3d maximum shear stress tracing line is discussed based on cobevel method

    摘要利用換法證明了一般三維塑性流動問題任意點應力狀態,可以完全由三維最大剪應力跡線上的信息確定,進而利用斜面法給出了三維塑性流動問題沿最大剪應力跡線正應力的化規律。
  7. Abstract : the information along 3d maximum shear stress tracing line is completely ascertained with the method of parameter transformation, then the changing rule of the normal stress along 3d maximum shear stress tracing line is discussed based on cobevel method

    文摘:利用換法證明了一般三維塑性流動問題任意點應力狀態,可以完全由三維最大剪應力跡線上的信息確定,進而利用斜面法給出了三維塑性流動問題沿最大剪應力跡線正應力的化規律。
  8. After that, on the non - inertial coordinate, the other part flow field, of the complex cylinder, which is composed of three basic flow field, is simulated by the same method as above

    然後,在非慣性系下,對具有兩個動邊界一個定邊界的多級缸上一級流場,採用投影法加換,在有邊界上耦合的方法進行求解。
  9. The experimental and computational results agree well with each other. the conclusion is that the proposed method, i. e., to divide a complex - cylinder flow field into basic flow field, and then to solve them respectively and coincide them on the common boundary, is a good way to simulate the whole flow field. further more, to solve basic flow field with the project method and coordinate transformation is suitable

    實驗表明:理論計算是可靠和正確的;投影法結合換法是求解基本動邊界流場的有效方法;基於基本流場的求解,將復雜流場分解為幾個基本流場,分別求解,然後在其有邊界上將涉及的基本流場耦合迭代,直到物理參數一致,是求解某些復雜動邊界流場的可行方法。
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