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概述了倾斜转弯(BTT)控制导弹的协调式自动驾驶仪系统的基术设计原理,同时也讨论了一般的设计思想、设计目的和要求、设计方法及性能分析。对飞行条件范围相当宽和闭合回路特征值的配置变化较小的导弹而言,所得到的控制规律组成的闭合回路系统是稳定的。给出了在最终阶段时6个飞行条件的控制回路频率响应,以表明反馈控制器设计的强壮性。踪跟系统的时间响应仿真证明,跟踪自动驾驶仪具有良好的转弯协调特性。
The basic design principle of the coordinated autopilot system for Tilt Turning (BTT) -controlled missiles is outlined. The general design concept, design goals and requirements, design method and performance analysis are also discussed. For missiles with a wide range of flight conditions and small variations in the configuration of closed loop eigenvalues, the resulting closed-loop system of control laws is stable. The control loop frequency response of 6 flight conditions at the final stage is given to show the robustness of the feedback controller design. Simulation of the time response of the tracking system proves that the tracking autopilot has good turning coordination characteristics.