摘要
针对飞行控制系统控制器参数优化问题,提出了一种基于小生境遗传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。
To optimize the parameters of the aircraft's flight control system(FCS), a reference model method based on the niche genetic algorithm(NGA) is proposed in this paper. To test the validity of this method, a simulation on a kind of aircraft' s lateral flight control system is made. It is showed that the method can tune the parameters of the FCS, and converge faster, and be programmed simply.
出处
《飞行力学》
CSCD
北大核心
2007年第3期79-82,86,共5页
Flight Dynamics