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)空間表達式形式的動力學方程，計算了縱列式直升機非耦合運動狀態(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構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，利用振型向量與質量陣和剛度陣的正交性，得到解耦的運動方程。先求出廣義激勵下各模態(tài)的響應，然后疊加起來得到系統(tǒng)的總響應。