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本方法用以计算带自动器的飞机飞行品质。计算包括两部分。第一部分系对系统在不同的控制输入和扰动输入下进行数字模拟计算。该计算可以包括系统中的非线性因素。第二部分系求解简化的常系数线性系统特征矩阵的特征根。本方法曾用于对带АП-155自动驾驶仪的例题飞机进行过计算。两部分计算结果基本一致。且与实物模拟计算吻合得较好。
This method is used to calculate the flight quality of an aircraft with a robot. The calculation consists of two parts. The first part simulates the system under different control input and disturbance input. This calculation can include non-linear factors in the system. The second part is the eigenvalue of the simplified linear system characteristic matrix with constant coefficients. This method was used to calculate the example aircraft with the АП-155 autopilot. Two parts of the calculation results are basically the same. Which is in good agreement with the physical simulation.