高速飞行器编队有限时间逆优化复合控制

doi:10.7527/S1000-6893.2025.32952

Abstract

Abstract:

To meet the performance requirements of rapid convergence of cooperative errors for high-speed aircraft formation， a finite-time inverse optimization composite control strategy is proposed. Firstly， the dynamic model of the high-speed aircraft is simplified， and a second-order system model along with a formation error dynamic model is established. Then， a sliding mode control method with finite-time convergence is designed to enhance the convergence speed of cooperative errors in high-speed aircraft formation， thereby meeting the real-time requirements of cooperative control during rapid maneuvers. To further enhance the cooperative performance on the basis of finite-time convergence， an inverse optimization composite control method is proposed to satisfy specified optimal performance metrics. Finally， simulation experiments verify the effectiveness and feasibility of the proposed finite-time inverse optimization composite control method.

Key words: high-speed aircraft formation, cooperative control, finite-time control, inverse optimization control, sliding mode control

CLC Number:

V249

Jinli GUO, Mou CHEN. Finite-time inverse optimization composite control of high-speed aircraft formation[J]. Acta Aeronautica et Astronautica Sinica, 2026, 47(S1): 732952.

Figures/Tables 9

Fig.1

Fig.2

Fig.3

Table 1

Initial states of followers

$x i, y i, z i / m$	$V i / (m · s - 1)$	$o i / m$	$ϕ i / r a d$	$χ i / r a d$
$0,29 000,31 610$	$1 700$	$600$	$- 0.499 π$	$0$
$0,29 605,29 500$	$1 700$	$4002$	$π / 4$	$π / 3$
$0,29 990,29 009$	$1 700$	$4002$	$π / 4$	$π / 3$

Table 1

Table 2

Convergence time with/without finite-time control strategy

变量	收敛时间/s
变量	未加入有限时间控制	加入有限时间控制
$p ˜ t$	6.5	4.4
$v ˜ t$	7.5	5.1

Table 2

Fig.4

Fig.5

Fig.6

Fig.7

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Finite-time inverse optimization composite control of high-speed aircraft formation

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