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解决了机动再入飞行器在气动系数变化范围大和气动耦合严重等恶劣条件下的姿态和过载控制问题 .为了能充分利用飞行器可测量信息提高系统自适应能力 ,提出了滚动通道状态方程参数辨识—级点配置—前馈补偿自适应控制和横向通道基于攻角反馈以过载为主控信号的变参数自适应控制的自动驾驶仪设计方法 .通过对某飞行器的制导控制系统仿真 ,可以看出该自动驾驶仪使飞行器有很好的飞行性能 .
In order to make full use of the measurable information of aircraft to improve the adaptive capability of the system, the parameter identification of the equation of state of the rolling passage is put forward, that is to say, the level of the aerodynamic coupling coefficient Point configuration-adaptive control of feedforward compensation and autopilot design method of adaptive adaptive control of transverse channel based on angle of attack feedback with overload as the main control signal.According to the guidance control system simulation of an aircraft, it can be seen that the automatic The pilot gives the aircraft good flight performance.