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研究机动再入飞行器的制导控制问题。为了解决机动再入飞行器气动系数变化范围大、气动耦合严重和气动参数非线性过零常值大等恶劣条件下的控制 ,并且能充分利用飞行器可测量信息提高系统自适应能力 ,本文提出了状态方程参数辨识—极点配置—前馈补偿自适应控制的飞行控制系统的设计方法。通过对新型号再入飞行器的制导系统仿真 ,可以看出该控制系统使其有很好的飞行性能
Research on Maneuvering Reentry Vehicle Guidance and Control Problem. In order to solve the harsh conditions such as the large range of aerodynamic coefficients of the reentry vehicle, the severe aerodynamic coupling and the large value of non-linear zero-crossing of aerodynamic parameters, and to make full use of the measurable information of the aircraft to improve the adaptive capability of the system, PARAMETER IDENTIFICATION - Pole Configuration - Feedforward Compensation Adaptive Control of Flight Control System Design Method. By simulating the guidance system of the new reentry vehicle, it can be seen that the control system has good flight performance