A method to reduce the static error and output impedance by biasing the TL431 is given.
给出了一种通过偏置tl 431来减小静态误差和输出阻抗的方法。
Output error method is one of the most widely applied methods in the region of aerodynamic parameter identification for aircraft.
输出误差法是飞行器气动参数辨识最广泛采用的一种方法。
It has been proved that satisfactory results can be easily obtained by using this process than the general output error method.
由计算结果的分析比较可知，扩充混合型法比一般的输出误差型法更为通用。
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