基于PID切换控制的弹道修正引信滚转角控制方法

Trajectory Correction Fuze Roll Angle Control Based on PID Switching Control Missile

  • 摘要: 为解决弹道修正引信在修正过程中弹体受力变化较大引起的模型非线性问题,为保证滚转角控制算法的有效控制范围可有效覆盖整个修正控制过程,采用了基于动压变化的位置−速度双闭环比例−积分−微分(proportional-integral-differential, PID)切换控制算法. 在传统PID控制算法基础上引入切换控制,将PID控制系统设计成子系统,依靠引信动力学模型与动压之间的关联,以动压为切换信号制定切换规则将多个PID控制系统串联,拓宽了滚转角控制系统的有效控制范围. 结合理论分析与仿真验证,结果表明:在整个弹道修正控制过程中定位精度在0.25°以内,响应时间小于0.3 s,验证了基于动压变化的PID切换控制算法对非线性的引信滚转角控制模型、持续滚转角控制的可行性.

     

    Abstract: To tackle the model nonlinear problem caused by huge force change of the ballistic correction fuse in the correction process, and to ensure that the effective control range of the roll angle control algorithm can effectively cover the entire correction control process, a position-velocity double closed-loop PID switching control algorithm based on dynamic pressure change was proposed. Based on the traditional PID control algorithm, switching control was introduced and PID control system was designed as a subsystem. Depending on the correlation between fuze dynamic model and dynamic pressure, switching rules were formulated with dynamic pressure as switching signal to connect several PID control systems in series, which expanded the effective control range of roll angle control system. In order to increase the stability of switching control, a gain scheduling control method was added. Combined with theoretical analysis and simulation verification, the results show that the positioning accuracy in the whole trajectory correction control process is less than 0.25°, and the response time is less than 0.3 s, which verifies the feasibility of PID switching control algorithm based on dynamic pressure change for the nonlinear fuze roll angle control model.

     

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