| 摘要 |
PURPOSE: To improve the response and the turning capacity of an airframe by suppressing the influence of an attitude angle speed to a guide signal. CONSTITUTION: A signalσ1 obtained by multiplying a tracking error by a gain is passed through a high-pass filter 7, a rate sensor output angle speed signalσ2 is passed through a low-pass filter 8, the output signals of the filters 7, 8 are added by an adder 9 as a guide signal to suppress the influence of the attitude angle speed for the guide signal, thereby improving the response and the turning capacity of an airframe.
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