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基于遗传算法的火箭转塔伺服系统最优PID控制研究
Optimal PID Control Research of Rotational Servo System for Multiple Rocket Based on Generic Algorithm
【摘要】 文中对某火箭发射装置的模拟位置伺服控制系统进行了研究。针对系统进行了建模和相关参数的计算;最后对系统进行仿真,得到基于遗传算法的最优的控制器参数K_p,K_i,k_d,。仿真结果表明,基于遗传算法的PID控制器可以实现工程的性能指标要求,具有很好的效果。
【Abstract】 An imitation of rotational servo system for rocket launch system is studied in this paper.Aimed at the a-c system,we construct the model and calculate interrelated control parameters.Finally,we take simulation on the system and get optimal parameters K_p,K_i,K_d based on Generic Algorithm.Simulation results indicate that this kind of PID controller can realize the properties request in engineering and achieve fairly good effects.
- 【文献出处】 弹箭与制导学报 ,Journal of Projectiles,Rockets,Missiles and Guidance , 编辑部邮箱 ,2006年S4期
- 【分类号】V448
- 【被引频次】8
- 【下载频次】96