考虑舵面效能损失的着舰主被动复合容错控制研究

周大鹏; 甄冲; 曲晓雷; 罗斐

doi:10.7527/S1000-6893.2026.32544

航空学报 >

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DOI: https://doi.org/10.7527/S1000-6893.2026.32544

考虑舵面效能损失的着舰主被动复合容错控制研究

周大鹏 ,
甄冲 ,
曲晓雷 ,
罗斐

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1. 沈阳飞机设计研究所
2. 西北工业大学
3. 中国航空工业集团公司沈阳飞机设计研究所
4. 大连理工大学

收稿日期: 2025-07-10

修回日期: 2026-02-10

网络出版日期: 2026-02-27

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Research on Hybrid Active-Passive Fault-Tolerant Control for Carrier Land-ing Subject to Control Surface Effectiveness Loss

ZHOU Da-Peng ,
ZHEN Chong ,
QU Xiao-Lei ,
LUO Fei

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Received date: 2025-07-10

Revised date: 2026-02-10

Online published: 2026-02-27

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摘要

在舰载机着舰过程中，受复杂恶劣的海面环境、甲板运动及舰艉流等强干扰影响，舵面故障的概率显著增加，可能导致着舰控制精度下降，甚至引发瞬时失稳等问题。本文融合被动容错控制与主动容错控制的优点，提出一种基于直接升力模式的主被动复合容错飞行控制方法。首先，针对舵面故障初期舰载机响应特性突变的问题，设计基于预定义时间全局快速终端滑模的被动容错控制方法，保证舰载机在预定时间内的飞行瞬时稳定性，并提升控制系统的鲁棒性。然后，针对着舰末段的高精度控制需求，设计基于在线辨识的主动自适应重构控制，增强舰载机故障后的姿态和航迹跟踪控制能力。最后，通过数学仿真及工程应用性仿真试验，验证该方法在升降舵和襟翼损伤故障情况下的的有效性。仿真结果证明，在不同舵面损伤程度下，该方法相比直接升力PID着舰控制方法及单一被动或主动容错控制，具有更强的鲁棒性和控制性能。

关键词： 直接升力着舰; 主被动复合容错控制; 滑模控制; 自适应控制; 舵面损伤

本文引用格式

周大鹏 , 甄冲 , 曲晓雷 , 罗斐 . 考虑舵面效能损失的着舰主被动复合容错控制研究[J]. 航空学报, 0 : 1 -0 . DOI: 10.7527/S1000-6893.2026.32544

Abstract

In the process of carrier-based aircraft landing, the probability of rudder failure increases significantly due to the strong interference of complex and harsh sea surface environment, deck movement and ship stern flow, which may lead to the decrease of landing control accuracy and even cause instantaneous instability. This paper combines the advantages of passive fault-tolerant control and active fault-tolerant control, and proposes an active-passive com-posite fault-tolerant flight control method based on direct lift mode. Firstly, aiming at the problem of sudden change of response characteristics of carrier-based aircraft in the early stage of rudder failure, a passive fault-tolerant con-trol method based on predefined time global fast terminal sliding mode is designed to ensure the instantaneous flight stability of carrier-based aircraft in a predetermined time and improve the robustness of the control system. Then, aiming at the high-precision control requirements of the terminal landing, an active adaptive reconfigurable control based on online identification is designed to enhance the attitude and track tracking control ability of the car-rier-based aircraft after failure. Finally, the effectiveness of the method in the case of elevator and flap damage is verified by mathematical simulation and engineering application simulation test. The simulation results show that the proposed method has stronger robustness and control performance than the direct lift PID landing control meth-od and single passive or active fault-tolerant control under different degrees of rudder damage.

Key words： Direct lift landing; active-passive combined fault-tolerant control; sliding mode control; adaptive control; control surface damage

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