具有控制约束的最速驾驶仪设计

为了解决导弹控制系统设计过程中采用试凑法进行参数设计周期太长以及执行机构饱和约束不易加入的问题．提出一种建模思想。将控制系统设计问题变为有约束优化问题。把系统的性能指标和执行机构饱和约束转化为约束条件。上升时间作为目标函数．采用逐次逼近法来进行迭代，直到得到满足约束的控制器参数。此方法能够直观地引入各种约束。并能够有效缩短导弹控制系统设计周期。

Control System Fast Response Design with Control Constraint

In order to reduce the period of autopilot design and to consider the saturation of the rudder angle, a new method is researched. In the model, the performance criteria and the saturation of the rudder angle are converted into constraints, and the rise time is translated into object, then use the constrained nonlinear optimization to find the control parameter. This method can add the constraint to the model directly and reduce the design period of control system.