linearized equation 中文意思是什麼
linearized equation
解釋
線性化方程- linearized : 線性化的
- equation : n. 1. 平衡,均衡;平均,相等。2. 【數學】方程式,等式。3. 【天文學】(時)差;均分,等分。4. 【化學】反應式。
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To see what error was engendered in the process, we now allow ni to differ from ne and use the linearized poisson equation.
為了研究在這個過程中引起了多少誤差,我們讓ni與ne不相同,並用線性化的泊松方程。 -
The equation of motion is linearized near the equilibrium position of the tethered mass system
基於小擺角假設,將系統運動微分方程在平衡位置附近線性化。 -
The dynamic model of induction motor under - reference frame is approximated by its associated discrete circuit model with the trapezoidal algorithm, after linearized using the neoton - rapson algorithm, the contribution of induction motor model to the circuit " s nodal equation matrix is calculated
按照改進節點法的要求,異步電機採用-坐標系下的動態模型,使用梯形法求解微分方程,經過離散化和線性化,得出異步電機作為一個電路元件對電路矩陣方程的貢獻。 -
At first, the original system with twelve - order differential equation is linearized to a six - order system by the dfl theory, and then control laws are designed by classical control method
首先以飛機原始非線性十二階微分方程為對象,利用直接反饋線性化( dfl )理論對飛機原始非線性方程進行線性化,將原系統等效於一個六階的線性系統。 -
In chapter 3, the non - linear equation was linearized with the jacobi matrix, and then the linearized equation was transformed into fixed frame to analyze the stability problem with eigenvalue method ( on - ground or hovering ) or floquet theory ( forward flight ). meanwhile, the equation was perturbed by sweep frequency excitation from steady state to get transit decay of lag response which was then transformed into fixed frame with a numerical fourier coordination transformation ( fct ). the fixed frame response along with the body response was analyzed via an fft to determine modal frequencies
然後,在穩態響應的基礎上利用雅各比矩陣對非線性方程進行了線化,線化后的方程利用多槳葉坐標變換轉換到固定系下后,利用直接特徵值分析(地面、懸停)或floquet理論(前飛)對系統進行了穩定性分析;同時,對系統進行了瞬態響應分析;在系統達到穩態的基礎上進行掃頻激勵,用fft變換求得系統頻率,進而用移動矩形窗方法分析得到系統的阻尼。 -
As the complexity of flight tasks increases, the linearized equation based on the small disturbance theory is no longer adequate for the design of control systems, and the necessity of exploring a nonlinear approach seems increasingly obvious
隨著飛機飛行任務不斷趨向復雜化,基於小擾動線性化方程的線性系統設計方法已經難以滿足現代飛機飛控系統的設計要求。這就迫使我們研究飛機的非線性控制律的設計方法。 -
In this paper, deconvolution and linearized inversion of receiver function are improved ; multi - channel deconvolution and wavelet inversion are developed for receiver function. the elastic wave motion equation is applied in the simulation and migration of receiver function in lateral inhomogeneous media, multi - grid algorithm is introduced in numerical modeling of elastic wave motion equation, and phase - delay boundary condition is also provided to absorb boundary reflection
在此基礎上,重點研究和發展了橫向非均勻介質中,基於波動方程的數值模擬與偏移成像方法,首次將多重網格演算法引入到彈性波方程的數值模擬和接收函數的偏移成像,還發展了一種延遲邊界方法,以消除人為邊界反射的影響。 -
Simulation results indicate that the drnn identifier is more accurate than the traditional ked theoretical model. ( 5 ) with reference to the parameter estimation problem, a linearized model of the experimental mechanism is established, whose state equation is determined by means of the continuous hopfield neural networks ( hnn )
5 .在參數估計方面,本文構造了彈性連桿機構動力學系統的線性化模型,根據連續型hopfield神經網路( hnn )的優化計算原理,對該線性化模型的狀態方程進行了參數估計。 -
The other algorithms is to linearized the state equation based on the command quaternion
另外一種是基於命令四元數對狀態方程進行線性化。 -
This paper presents and probes into several filtering schemes for the deep space explores attitude measurement system composed of star sensors and gyros. under the stellar - inertial modes, two attitude determination algorithms are designed which use the extended kalman filter. one of the algorithms is to linearized the state equation based on the optimal estimation
本文中以星敏感器和光纖陀螺為基本配置組成的深空探測器姿態測量系統為對象,針對星敏感器與光纖陀螺聯合定姿模式和基於星敏感器的定姿模式,對深空探測器的三軸姿態濾波技術方案進行了設計與研究。 -
On the controlling of besiding, a trailing pid method is introduced. concrete step is that dividing a step period into many consective space by time, secondly, linearizing the dynamic equation of besiding in each space ; then, pid method was use in every linearized space. this method attains the aim of controlling more easily and precisely
在besiding機器人的控制問題上,文章採用的是跟蹤式的pid控製法,具體措施是首先把機器人的行走過程按一個很小的時間區間分成許多時間域,其次把機器人的力學方程在每個時間領域里線性化,然後在這個時間域內對機器人進行pid控制。 -
The nonlinear equation of aircraft is linearized by state transforming differential relationship between input and a new input, and the nonlinear system is decoupled to a one order linear system and a two order linear system
通過狀態變換輸出與新輸入間的線性微分關系使非線性飛機方程反饋線性化,將原非線性系統解耦為一個一階和一個二階線性系統。
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