The proposed method is applied to satellite attitude controller design to cope with the errors arising while linearization procedure.

将所得结果应用于卫星姿态控制系统的设计，以解决对模型进行线性化处理时产生的误差。

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By means of the feedback linearization procedure of differential geometry, an equivalent, fully controllable and linear model was derived via a homomorphic transformation for the AMT clutch system.

进一步应用基于微分几何的反馈线性化方法，将原非线性系统等价为完全可控型线性化模型。

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