uncoupled mode

基本解釋

The stability roots of the tandem helicopter in the uncoupled mode were computed using the dynamic equations in the state-space form.
采用狀態(tài)空間表達(dá)式形式的動力學(xué)方程，計(jì)算了縱列式直升機(jī)非耦合運(yùn)動狀態(tài)下的穩(wěn)定根；
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A relatively uncoupled mode-superposition method and a modified first-order perturbation method are derived. A numerical example shows that the present strategy is correct and effective.
最后通過算例證明，提出的基于攝動法及等效線性化的耗能減震結(jié)構(gòu)振型分解法是行之有效的。
Uncoupled differential equations of motion were obtained by utilizing the modal transformation and the orthogonality of the mode shapes with respect to the mass and stiffness matrices.
通過模態(tài)變換，利用振型向量與質(zhì)量陣和剛度陣的正交性，得到解耦的運(yùn)動方程。先求出廣義激勵下各模態(tài)的響應(yīng)，然后疊加起來得到系統(tǒng)的總響應(yīng)。