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Fermelia A. Gyorog D.A. Flanigan V.J. 《IEEE transactions on aerospace and electronic systems》1976,(6):767-782
The nonlinear set of equations which represent helicopter motion is linearized about a prescribed nominal state. Once the linearized system is obtained it is validated by comparing the output of the nonlinear system to that of its linearized counterpart. Having obtained a linear model, linear system theory may then be applied in order to investigate the stability and control characteristics of the aircraft. 相似文献
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