Design And Simulation of TS Fuzzy Based Cooperative Control of Missile Formation

doi:10.16182/j.issn1004731x.joss.21-0146

Abstract

Abstract:

Aiming at the requirement of cooperative operation of multi-missile formation, a cooperative control algorithm of multi-missile formation based on Takagi-Sugeno(TS) fuzzy control theory is proposed.The flight speed, trajectory angle and trajectory deflection angle of the missile are taken as parameters in the leader-follower mode missile formation flying system.The local asymptotically stable controller is designed by using the systemlocal linearization of multiple groups of equilibrium pointsduring the whole flight process.Through the expert experience method,the membership function and fuzzy rules for the system are designedwith TS fuzzy theory, and the whole multi-missile cooperative control system is completed and the stability of the system is proofedby relevant simulation verification.Simulation result shows that TS fuzzy control improves the robustness of the system.

Key words: multi-missile cooperation, piecewise linearization, TS fuzzy control, anti-interference

CLC Number:

TP271+

Yexin Zhang, Yu Cheng, Hongyan Yan, Xuwei Fan, Xu Zhang, Yi Tian. Design And Simulation of TS Fuzzy Based Cooperative Control of Missile Formation[J]. Journal of System Simulation, 2022, 34(7): 1559-1567.

Figures/Tables 11

Fig. 1

Fig. 2

Table 1

Working point of controlled object.

_工工作点

模糊子集

Δ X 1

-1

-0.4

-0.1

0.1

0.4

Δ X 2

-0.8

-0.5

-0.4

0.4

0.5

0.8

Δ X 3

-1

-0.6

-0.3

0.3

0.6

Table 1

Fig. 3

Fig. 4

Fig. 5

Table 2

Fig. 6

Fig. 7

Fig. 8

Fig. 9

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状态	从弹1	从弹2
相对坐标系下初始位置/m	x=400	x=460
	y=-480	y=-520
	z=300	z=-250
相对坐标系下期望位置/m	x=600	x=600
	y=-350	y=-350
	z=400	z=-400
初始速度/(m·s^-1)	150	165
初始弹道倾角(°)	3.5	-5.6
初始弹道偏角(°)	4	6.2

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