非柔性控制 的英文怎麼說

中文拼音 [fēiróuxìngkòngzhì]
非柔性控制 英文
non-flexible control
  • : Ⅰ名詞1 (錯誤) mistake; wrong; errors 2 (指非洲) short for africa 3 (姓氏) a surname Ⅱ動詞1 ...
  • : Ⅰ形容詞1 (軟) soft; supple; flexible 2 (柔和) gentle; yielding; mild Ⅱ動詞1 [書面語] (安撫)...
  • : Ⅰ名詞1 (性格) nature; character; disposition 2 (性能; 性質) property; quality 3 (性別) sex ...
  • : 動詞1 (告發;控告) accuse; charge 2 (控制) control; dominate 3 (使容器口兒朝下 讓裏面的液體慢...
  • : Ⅰ動詞1 (製造) make; manufacture 2 (擬訂; 規定) draw up; establish 3 (用強力約束; 限定; 管束...
  • 柔性 : flexibility
  • 控制 : control; dominate; regulate; govern; manage; check; cybernate; manipulate; encraty; rule; rein; c...
  1. Non - collocated model reference adaptive control for flexible manipulator arm

    機械臂並置式模型參考自適應
  2. However, due to the elastic deflection and vibration of the links, the flexible manipulator becomes an infinite dimension mimo system with distributed parameters, and is highly nonlinear and strong coupling. therefore, the model and the control of flexible manipulator are of great significance both in theory and in application

    然而也正是由於連桿存在彈變形和振動,使得機械手成為一個高度的、分佈參數的、強耦合的無窮維多輸入多輸出系統, ,因此其建模和也具有重要的理論意義和應用前景。
  3. Firstly, in order to treat the local weakened effect of the crack on the shaft, the equivalent line - spring model is built. then the constitutive equations are derived and the flexibility model of the rotating shaft is discussed. based on the lagrange equations, the non - linear dimensionless differential equations of the single rotor system with the disk and crack located at an arbitrary position of the shaft are obtained

    首先為處理裂紋對軸的局部削弱作用,提出了等效線彈簧模型,推導了線彈簧彈本構關系,獲得了裂紋轉動軸的度模型,然後,應用lagrange方程建立了盤和裂紋處于軸任意位置的無量綱的單盤轉子系統的運動微分方程。
  4. The dynamics behaviors of the flexible jeffcott rotor system supported by unsteady short dynamic bearing are investigated. based on nonlinear unsteady - state dynamic n - oil film force model described by three functions the local stability of the periodic solutions with the controlling parameters, rotational speed ratio, imbalance amount, damping ratio and viscidity, are predicted by using the floquet multiplier. it is found that the period doubling bifurcation is caused by a certain imbalance amount and the hopf bifurcation is created by the lost stability of the oil - film

    研究了穩態動載短軸承支撐的jeffcott轉子系統的動力特,基於可用三個函數表示動態油膜的穩態油膜力模型,將轉速比、不平衡量、阻尼比、粘度作為參數,利用floquet乘子預測周期解的局部穩定,發現倍周期分叉是由一定量的不平衡引起的,而hopf分叉是由油膜失穩造成的。
  5. The dissertation refers to comparatively full literatures in the field of vsc, and the development history and characteristics of vsc are summarized, and the elementary concepts, elementary definitions, elementary properties, elementary principles and design methods are particularly introduced, and the causes of the chattering phenomenon are systematically analysed, and the study status of the chattering phenomenon and the main methods to eliminate the chattering are elaborated. for the deficiencies of traditionary methods, three improved methods are developed, which are improved exponent reaching law solution, variable boundary layer solution and the solution by adding an auxiliary continuous control term. for uncertain linear systems, an adaptive fuzzy integral variable structure control stategy ( afivsc ) is put forward to eliminate the chattering around the sliding plane, which introduces fuzzy logic to soften the non - linear discontinuous sig nal in the control variable and utilizes adaptive theory to adjust output membership function according to how much the uncertainty of the system is

    比較全面地查閱了關于變結構理論的文獻,總結了滑模變結構的發展歷史和特點,詳細介紹了變結構的基本概念、基本定義、基本質、基本原理以及設計方法;系統分析了變結構系統抖振產生的機理,並闡述了國內外目前對抖振問題的研究現狀以及消除抖振的主要方法;針對傳統抑和消除抖振方法的不足,改進了傳統方法,得到了三種新的消除抖振的方法? ?即改進的指數趨近律法、可變邊界層法和附加連續項法;針對不確定系統,在變結構策略中引入模糊邏輯和自適應理論來消除滑動平面上的抖振,提出了一種自適應模糊積分變結構方案( afivsc ) ,利用模糊邏輯來量中不連續部分,採用自適應理論,根據系統不確定大小在線調整模糊輸出量的隸屬函數,另外,鑒于模糊本質上是有靜差的,所以本文選擇了帶積分項的切換函數,由於積分項的存在使系統較正為無靜差系統。
  6. Firstly, a reduced order model of this flexible structure is obtained by frequency domain identification, then unstructured uncertainties constituted by neglected modes are taken care of in the time of design process by choosing appropriate weighting functions, arid finally a robust feedback controller is designed based on the reduced order model and the approximate knowledge of unmodeled uncertainties

    首先通過頻域辨識得到結構的降階模型,而剩餘高階模態構成的結構不確定,通過對權函數的選擇在設計階段就加以考慮,然後基於降階模型和未建模不確定的近似特設計了魯棒反饋器。
  7. But because of an indeterminate flexible structure with many degree of redundancy, its variant inner force under dead - loading, nonlinear behavior and the correlation between construction method and completed structure, especially incessant conversion of system in construction method, these must bring many complicated change to construction internal force and displacement. these main factors resulting in construction control analysis become more important in the design of cable - stayed bridge

    但由於它屬于高次超靜定的結構,恆載內力狀態具有多樣、結構狀態呈、施工過程與成橋狀態具有相關,特別是在施工階段結構體系的不斷轉換,必然給橋梁結構帶來較復雜的內力和位移變化,這些特點使得斜拉橋的施工分析成為突出的研究課題。
  8. Its new global dynamic model in terms of measured joints is derived by coordinate transformation, and the decoupled control equations for joint relative angles and elastic parts of the flexible manipulator are obtained with the model - based nonlinear decoupling feedback control method

    通過坐標變換,推導出一種新的以可測關節角為變量的全局動態模型,並在此基礎上運用基於模型的解耦反饋方法得到關節相對轉角與臂的彈變形部分解耦形式方程。
  9. Based on the nonlinear equilibrium equation of the cable - cabin system, a stationary model for position control of the flexible cable - cabin system with large span is established through optimal strategy on the distribution of the driving forces. thus the unlooped control of movement of the cabin is realized by adjusting the lengths of the cables coordinately

    在建立艙索系統靜平衡方程的基礎上,採取使驅動力均勻的優化配置策略,建立了大跨度艙索系統的穩態位置模型,實現了基於索長調整的饋源艙開環運動
  10. Active vibration control of a cantilever beam in non - inertial system

    系下懸臂梁的振動主動
  11. Flutter is the most important instable problem and it restricts the flight envelope and performance of a vehicle. aeroservoelasticity, including active flutter suppression technology, is a multidisciplinary optimization technology that studies the interaction of flexible structure, unsteady aerodynamics and flight control system

    以主動顫振抑系統設計為代表的氣動伺服彈力學( ase )是一門涉及結構、飛行器運動引起的定常和定常氣動力以及飛行系統相互作用的多學科技術。
  12. The nonlinear dynamic control strategy of two - link flexible arm is analyzed

    摘要對雙連桿機械臂動力學問題進行了分析。
  13. By reason of its no - dependency on structure, the algorithm has importance for nonlinear structure and large flexible structure of which the model is difficult to obtain

    由於該演算法對結構的不依賴,對難以建模的結構和結構的振動主動具有實際意義。
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