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战斗机和空射诱饵的编队控制器仿真 被引量:5

Simulation of Formation Control of Fighter and Mald
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摘要 针对战斗机和空射诱饵伴随飞行中的编队控制问题,提出了一种采用相对误差的编队控制方法。首先建立了战斗机和空射诱饵的运动模型及相对运动模型,并参考虚拟长机的编队方法,将诱饵弹指定为长机,战斗机指定为僚机;然后建立了采用相对误差的编队控制器模型,并以空射诱饵质心干扰的顺利实施为前提,设定了控制器的约束条件;最后对编队控制器模型进行仿真分析,仿真结果表明设计的控制器可以对战斗机和空射诱饵的编队队形进行有效控制。 In view of the formation control problem of fighter and MALD in the process of accompanied flight, we proposed a new method for the formation control based on the relative error. Firstly, the motion model and the rela- tive motion model of the fighter and the MALD was established, and the MALD was specified as the leader while the fighter was the wingman based on the formation control method of virtual leader. Then the model of the formation con- troller based on the relative error was established, and the constraints was set to ensure the smooth implementation of the centroid jamming. Finally, the model of the formation controller was simulated and the results show that the con- troller designed is able to control the formation of the fighter and the MALD effectively.
出处 《计算机仿真》 CSCD 北大核心 2015年第8期49-53,145,共6页 Computer Simulation
关键词 战斗机 空射诱饵 相对误差 编队控制 Fighter MALD Relative error Formation control
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