基于离线网络/在线辨识的舰载机自抗扰控制

doi:10.7527/S1000-6893.2024.31317

Abstract

Abstract:

To address the high-precision landing control problem of carrier-based aircraft under complex environment and strong uncertainty， this paper proposes a direct lift mode active disturbance rejection control method based on offline neural network/online identification. Firstly， referring to the American ‘Magic Carpet’ control system and analyzing its key technical mechanism， the direct lift landing active disturbance rejection control method of carrier-based aircraft is designed. The extended state observer is used to estimate and compensate the total disturbance caused by gust disturbance and system uncertainty. Secondly， according to the evaluation criteria of landing control engineering performance index， the optimal control parameters are selected， and the neural network mapping relationship with flight model uncertainty as input and optimal landing control parameters as output is established. Finally， the active disturbance rejection control parameters are efficiently optimized by online identification. The simulation results show that the proposed method has higher robustness than the baseline controller， and can effectively improve the high-precision landing performance of carrier-based aircraft under interference conditions.

Key words: direct lift control, active disturbance rejection control, neural networks, Magic Carpet, online identification

CLC Number:

V249.1

Ming YAN, Jiaxing WANG, Heqi LI, Kai LIU. Active disturbance rejection control of carrier-based aircraft based on offline network/online identification[J]. Acta Aeronautica et Astronautica Sinica, 2025, 46(13): 531317.

Figures/Tables 17

Fig.1

Table 1

Airwake classification

艉流分类	自由大气紊流	稳态分量	周期分量	随机分量
水平方向	$u 1$	$u 2$	$u 3$	$u 4$
垂直方向	$w 1$	$w 2$	$w 3$	$w 4$

Table 1

Fig.2

Fig.3

Fig.4

Table 2

Control parameters

参数	取值	参数	取值
$K p γ$	20	$K d γ$	3
$K p α$	10	$K d α$	5
$K p V$	-0.55	$K d V$	-0.08
$K$	-0.4

Table 2

Fig.5

Table 3

Fig.6

Fig.7

Fig.8

Fig.9

Fig.10

Table 4

Fig.11

Fig.12

Fig.13

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仿真输入	数值
初始迎角/（°）	12.05
初始高度/m	500
配平速度/（m·s^-1）	80
相对航迹角/（°）	-4
绝对航迹角/（°）	3.83
航母甲板速度/（m·s^-1）	3.33

偏差项目	拉偏值
升力系数	±20%
升降舵舵效	±20%
俯仰力矩	±20%
襟翼舵效	±20%

Active disturbance rejection control of carrier-based aircraft based on offline network/online identification

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