基于粒子群优化算法的旋转导弹姿态修正策略
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摘要
针对某型无控火箭弹,对其进行制导化改造并设计了基于粒子群优化算法的直接力装置工作策略,建立弹体六自由度模型,并进行仿真分析,研究结果表明所设计的直接力点火策略能够保证弹体稳定的前提下,有效减小落点散布,为无控火箭弹制导化改造的控制策略设计及其工程化应用提供了参考。
This paper,with a certain type of rotating airframe missile as the research object,according to the missile dynamics and kinematics model,formed a model of missile with direct force device,and simulated the effect of particle swarm optimization control method in ballistic characteristic point. Result shows that the way in the paper can reduce the circular error probable. The result provides reference for engineering application.
This paper,with a certain type of rotating airframe missile as the research object,according to the missile dynamics and kinematics model,formed a model of missile with direct force device,and simulated the effect of particle swarm optimization control method in ballistic characteristic point. Result shows that the way in the paper can reduce the circular error probable. The result provides reference for engineering application.
引文
[1]张明星,黄晓霞.国外远程制导火箭弹技术现状与趋势[J].四川兵工学报,2013,34(7):59-62.
[2]李新国,方群.有翼导弹飞行动力学[M].西安:西北工业大学出版社,2005.
[3]杨军,杨晨,段朝阳,等.现代导弹制导控制系统设计[M].北京:航空工业出版社,2005.
[4]李永亮.十字形鸭翼布局旋转弹控制系统研究[D].南京:南京航空航天大学,2013.
[5]郭正玉,梁晓庚.弹道修正弹模糊自适应PID控制器设计[J].四川兵工学报,2014,34(4):1-4.
[6]毕艳超,姚晓先,宋晓东,等.双通道控制旋转导弹的舵机控制研究[J].弹箭与制导学报,2014,34(2):25-28.
[7]郑新,傅维贤,赵民.滚转弹道导弹运动规律与控制研究综述[J].航天控制,2011,32(4):37-39.
[8]任淼,王秀萍.国外空空导弹发展动态研究[J].航空兵器,2013,34(5):1-4.
[9]曹硕宏.基于柔性变结构控制理论的滚转导弹飞行控制系统设计[D].南京:南京理工大学,2013.
[10]郭正玉,梁晓庚.制导火箭弹修正方法和控制精度分析[J].计算机仿真,2015,32(9):91-94.
[11]PHILIPPE WERNERT.Stability analysis for canard guided dual-spin stabilized projectiles[C]//AIAA Atmospheric Flight Mechanics Conference and Exhibit.Chicago,Illinois,2009.
[12]ROGERS J,COSTELLO M.Design of a Roll-Stabilized Mortar Projectile with Reciprocating Canards[J].Journal of Guidance,Control,and Dynamics,2010,33(4):1026-1034.
[2]李新国,方群.有翼导弹飞行动力学[M].西安:西北工业大学出版社,2005.
[3]杨军,杨晨,段朝阳,等.现代导弹制导控制系统设计[M].北京:航空工业出版社,2005.
[4]李永亮.十字形鸭翼布局旋转弹控制系统研究[D].南京:南京航空航天大学,2013.
[5]郭正玉,梁晓庚.弹道修正弹模糊自适应PID控制器设计[J].四川兵工学报,2014,34(4):1-4.
[6]毕艳超,姚晓先,宋晓东,等.双通道控制旋转导弹的舵机控制研究[J].弹箭与制导学报,2014,34(2):25-28.
[7]郑新,傅维贤,赵民.滚转弹道导弹运动规律与控制研究综述[J].航天控制,2011,32(4):37-39.
[8]任淼,王秀萍.国外空空导弹发展动态研究[J].航空兵器,2013,34(5):1-4.
[9]曹硕宏.基于柔性变结构控制理论的滚转导弹飞行控制系统设计[D].南京:南京理工大学,2013.
[10]郭正玉,梁晓庚.制导火箭弹修正方法和控制精度分析[J].计算机仿真,2015,32(9):91-94.
[11]PHILIPPE WERNERT.Stability analysis for canard guided dual-spin stabilized projectiles[C]//AIAA Atmospheric Flight Mechanics Conference and Exhibit.Chicago,Illinois,2009.
[12]ROGERS J,COSTELLO M.Design of a Roll-Stabilized Mortar Projectile with Reciprocating Canards[J].Journal of Guidance,Control,and Dynamics,2010,33(4):1026-1034.