摘要
针对多导弹编队保持控制器设计展开研究。首先利用多智能体系统技术研究领弹与从弹的协同优化组织结构;其次针对面向编队飞行的从弹控制律和实现算法进行重点研究,利用惯性坐标系下从弹与领弹的坐标得到相对坐标差值,进一步利用误差的动力学特性设计了三维条件下基于从弹的稳定的编队控制器,实现对从弹的速度控制、弹道偏角控制和弹道倾角控制,在领弹机动情况下,从弹与领弹的相对距离始终为指定的期望值;最后通过仿真实验验证此编队控制器具有较强的鲁棒性和稳定性。
Design of multi-missile formation hold controller was involved.Firstly,the cooperative optimization structure using multi-agent system was carried out.Secondly,a nonlinear formation flight control algorithm for the leader-follower was addressed.The objective was to design a formation hold controller which the relative distance between the leader and the follower was closed to their desired values.Velocity control,flight path angle control and heading angle control were realized which based on a new error formulation in the inertial frame.At last,simulation results proved the formation controller was robustness and stability.
出处
《飞行力学》
CSCD
北大核心
2010年第3期69-73,共5页
Flight Dynamics
基金
航空科学基金和航空电子系统综合技术国防科技重点实验室联合资助(20095584006)
