基于性能函数的高速飞行器编队切换控制方法

doi:10.7527/S1000-6893.2025.32951

Abstract

Abstract:

For high speed aircraft formation switching systems， a performance function-based finite-time control method is proposed to achieve rapid and stable formation switching in dynamic mission scenarios. A formation dynamics model comprising a leader and followers is established， and a novel finite-time cooperative controller is designed to ensure rapid convergence to the desired formation in each mode. To address formation switching triggered by mission changes， a joint decision mechanism integrating performance functions and dwell-time constraints is introduced. This mechanism evaluates the system state in real-time and triggers formation switching only when both performance requirements are satisfied and dwell-time conditions are met， thereby ensuring smooth transitions and global switching. The results show that the proposed control method can ensure rapid convergence， global stability， and switching smoothness for high-speed aircraft formation switching.

Key words: high speed aircraft formation, finite-time, performance function, dwell time, formation switching

CLC Number:

V249

Qiaoqiao ZHENG, Mou CHEN. Formation switching control for high speed aircraft based on performance function[J]. Acta Aeronautica et Astronautica Sinica, 2026, 47(S1): 732951.

Figures/Tables 8

Fig.1

Fig.2

Fig.3

Table 1

Five HSAs initial states

HSA	$(p x i, p v i, p z i) / m$	$V i / (m · s - 1)$
HSA0	$(100,100,3 000)$	$1 020$
HSA1	$(450,98,3 000)$	$1 000$
HSA2	$(100, - 200,3 000)$	$970$
HSA3	$(97,500,3 000)$	$1 002$
HSA4	$(- 297,101,3 000)$	$1 000$

Table 1

Fig.4

Fig.5

Fig.6

Fig.7

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Formation switching control for high speed aircraft based on performance function

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