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本文利用极点配置的方法,研究了具有速率陀螺和线加速度计反货的Robust导弹的自动驾驶仪的设计,导出了设计公式,只要给出合适的极点位置,就可以得到自动驾驶仪的设计参数。利用该公式还能很容易地完成低频模型线性最优控制的自动驾驶仪设计。
In this paper, the design of the autopilot of Robust missile with speed gyro and line accelerometer counter-goods is studied by using the pole placement method. The design formula is derived. The design parameters of the autopilot can be obtained given the suitable pole position. . Using this formula, the autopilot design for linear optimal control of low-frequency models can also be easily accomplished.