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本文提出了一个用于飞行器稳定回路参数选择的快速估算方法,利用该方法可以在初步设计阶段,根据某些设计要求同时确定两个状态反馈系数。所给的算例表明,该方法十分简便,而且可以适用于某些广为应用的自动驾驶仪设计。
In this paper, a fast estimation method for the selection of parameters of aircraft stability loop is proposed. With this method, two state feedback coefficients can be simultaneously determined according to some design requirements in the initial design stage. The given examples show that this method is very simple and can be applied to some widely used autopilot designs.