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叙述了导弹制导与控制系统H_∞控制器的设计实例。简化线性时不变模型和六自由度非线性时变模型的仿真表明:在不改变系统其他元器件的情况下,与采用比例导引放大器相比较,采用H_∞控制器的制导与控制系统可以达到更好的性能和鲁棒性。
Describes the design of missile guidance and control system H_∞ controller design. The simulation results of the simplified linear time-invariant model and the six-degree-of-freedom nonlinear time-varying model show that the guidance and control system using H_∞controller can be compared with the proportional pilot amplifier without changing other components of the system Achieve better performance and robustness.