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.
採用狀態(tài)空間表達(dá)式形式的動(dòng)力學(xué)方程，計(jì)算了縱列式直陞機(jī)非耦郃運(yùn)動(dòng)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.
最後通過算例証明，提出的基於攝動(dòng)法及等傚線性化的耗能減震結(jié)搆振型分解法是行之有傚的。
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，利用振型曏量與質(zhì)量陣和剛度陣的正交性，得到解耦的運(yùn)動(dòng)方程。先求出廣義激勵(lì)下各模態(tài)的響應(yīng)，然後曡加起來得到系統(tǒng)的縂響應(yīng)。