摘要
针对飞行控制系统控制器参数优化问题,文中提出了一种基于粒子群算法的模型参考优化整定策略。并将此策略应用于某型飞机的横侧向飞行控制系统的参数优化之中,仿真结果表明,该优化策略能够有效地整定飞行控制系统的参数,具有收敛速度快,编程简单的优点。
In this paper, A reference model method based on the particle swarm optimization which is used for optimizing the parameters of the aircraft＇s flight control system. To test the validity of this method, a simulation on a kind of aircraft＇s lateral flight control system is made. It is shown that the method can tune the parameters of the FCS, and converge faster, simply programmed.
出处
《弹箭与制导学报》
CSCD
北大核心
2006年第4期79-81,共3页
Journal of Projectiles,Rockets,Missiles and Guidance
