不对称机翼损伤飞机特性分析与增量容错控制（先进飞行器安全控制专栏）

doi:10.7527/S1000-6893.2025.32501

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不对称机翼损伤飞机特性分析与增量容错控制（先进飞行器安全控制专栏）

李煜¹,²,陈家鑫¹,李珂澄¹,溫志湧²,李霓¹,刘小雄¹

1. 西北工业大学
2. 香港理工大学

收稿日期:2025-07-01 修回日期:2025-09-14 出版日期:2025-09-18 发布日期:2025-09-18
通讯作者: 刘小雄
基金资助:
国家自然科学基金;国家自然科学基金;航空科学基金

Analysis of aircraft characteristics with asymmetric wing damage and incremental fault-tolerant control

Received:2025-07-01 Revised:2025-09-14 Online:2025-09-18 Published:2025-09-18

摘要/Abstract

摘要： 为了提高机翼损伤飞机的安全飞行能力，本文开展了不对称机翼损伤对飞机气动和动力学特性的影响研究，并提出一种基于快速预定义时间的增量控制方法，以增强损伤飞机的稳定恢复能力和容错控制性能。首先，借助CFD软件分析了锯齿形和穿孔形机翼损伤对飞机气动特性的影响；其次，根据损伤影响特性，建立了不对称机翼损伤飞机的非线性六自由度动力学和动力学模型，研究了三种典型损伤飞机的配平策略，并根据配平实例探讨了其适用范围；随后，改进了现有预定义时间控制理论，进一步提升了闭环系统收敛速度，解决了收敛时间和用户设定时间不匹配以及收敛边界不可调的问题。在此基础上，基于快速预定义时间理论设计了增量容错控制器，并通过Lyapunov方法证明了闭环系统在机翼损伤下的稳定性和预定义时间收敛特性；最后，通过数字仿真和实时仿真实验验证了所设计增量轨迹容错控制器的有效性，并通过对比验证了其优越性。

关键词: 不对称机翼损伤, 损伤飞机配平, 快速预定义时间控制, 增量容错轨迹控制, 实时仿真实验

Abstract: To enhance the flight safety of aircraft with wing damage, this paper investigates the aerodynamic and dynamic characteristics of asymmetric wing damage and proposes an incremental fault-tolerant control method based on an improved predefined-time theory. First, CFD calculations are conducted to analyze the effects of wing-tip truncation and perforation damage on aerodynamic performance. Based on the above aerodynamic characteristics, a six-degree-of-freedom nonlinear model of the aircraft with asymmetric wing damage is established. Three representative trim strategies are then analyzed, and their applicability is discussed through comparative case studies. Subsequently, the existing prede-fined-time control theory is improved to accelerate convergence and address the mismatch between theoretical convergence time and user-defined time. On this basis, an incremental fault-tolerant controller is developed for the damaged aircraft, and the stability and predefined-time convergence of the closed-loop system under wing damage are rigorously proven using Lyapunov theory. Finally, the effectiveness and superiority of the proposed incremental trajectory fault-tolerant control scheme are validated through both numerical simulations and real-time experiments.

Key words: Asymmetric wing damage, Trim strategy of damaged aircraft, Fast predefined-time control, Trajectory incremental fault-tolerant control, Real-time simulation experiments.

中图分类号:

V249.1

李煜陈家鑫李珂澄溫志湧李霓刘小雄. 不对称机翼损伤飞机特性分析与增量容错控制（先进飞行器安全控制专栏）[J]. 航空学报, doi: 10.7527/S1000-6893.2025.32501.

参考文献

[1] LI Y, WEN C Y, LIU X X, et al. Prescribed-Time Fault-Tolerant Flight Control for Aircraft Subject to Structur-al Damage [J]. IEEE Transactions on Aerospace and Electronic Systems, 2025, 61(2): 1848-1859.
[2] SHAH G H. Aerodynamic effects and modeling of dam-age to transport aircraft[C]// AIAA Atmospheric Flight Mechanics Conference and Exhibit. 2008.
[3] GENG Y S, PANG B, Liu Y S, et al. Aerodynamic per-formance analysis of different damaged types of a tur-boprop wing[J]. Journal of Mechanics, 2025, 41, 192-202.
[4] KRZYSIAK A. Wind tunnel tests of damage to the tu-154M aircraft wing[J] Journal of Aerospace Engineer-ing, 2019, 32(6), 04019083.
[5] BACON B J, GREGORY I M. General Equations of Motion for a Damaged Asymmetric Aircraft[C]// AIAA Atmospheric Flight Mechanics Conference and Exhibit. 2007.
[6] LI Y, LIU X X, MING R C, et al. A cascaded nonlinear fault-tolerant control for fixed-wing aircraft with wing asymmetric damage[J]. ISA Transactions, 2023, 136, 503-524.
[7] GUO J X, TAO G, LIU Y. Multivariable Adaptive Con-trol of NASA Generic Transport Aircraft Model with Damage[J]. Journal of Guidance, Control, and Dy-namics, 2011, 34(5), 1495-1506.
[8] ZHANG Y M, JIANG J. Bibliographical review on re-configurable fault-tolerant control systems[J] Annual Reviews in Control, 2011, 32(2), 229–252.
[9] DU Z H, LYU Y X, ZHAI X H, et al. Fault-Tolerant Control for Fixed-Wing Aircraft with Asymmet-ric Damage: Model, Method, and Experiment[J]. Jour-nal of Guidance, Control, and Dynamics, 2025, 48(5), 1004-2024.
[10] ZHANG J, YANG X K, YANG L Y. Virtual-command-based model reference adaptive control for abrupt struc-turally damaged aircraft[J] Aerospace Science and Technology, 2018, 78, 452-460.
[11] 王乾, 李清, 程农, 等. 一种针对结构损伤的非线性容错飞行控制方法[J]. 航空学报, 2016, 37(2): 637-647.
WANG Q, LI Q, CHENG N, et al. A nonlinear fault tol-erant flight control method against structural damage[J]. Acta Aeronautica et Aeronautica Sinica, 2016, 37(2): 637-647 (in Chinese).
[12] SIEBERLING S, CHU Q P, MULDER J A. Robust Flight Control Using Incremental Nonlinear Dynamic Inversion and Angular Acceleration Prediction[J]. Jour-nal of Guidance, Control, and Dynamics, 2010, 33(6), 1732-1742.
[13] 党小为, 唐鹏, 孙洪强, 等．基于角加速度估计的非线性增量动态逆控制及试飞[J]. 航空学报, 2020, 41(4): 323-534
DANG X W, TANG P, SUN H Q, et al. Incremental non-linear dynamic inversion control and flight test based on angular acceleration estimation [J]. Acta Aeronautica et Aeronautica Sinica, 2020, 41(4), 323-534.
[14] 李煜，陈通文，王志刚，等．基于预设时间的直接升力着舰增量控制方法[J]．航空学报, 1-18 [2025-06-24]. https://hkxb.buaa.edu.cn/CN/10.7527/S1000-6893. 2024.31163
Li Y, CHEN T W, WANG Z G, et al. Research on incre-mental control of direct lift landing based on prede-fined-time theory[J]. Acta Aeronautica et Astronautica Sinica, 1-18 [2025-06-24]. https://hkxb.buaa.edu.cn/CN/10.7527/S1000-6893.2024.31163 (in Chinese).
[15] 邹雨春, 陶呈纲, 甄子洋, 等. 基于直接力的飞翼布局舰载机精确着舰控制[J]．航空学报, 1-18 [2025-06-24]. https://hkxb.buaa.edu.cn/CN/10.7527/S1000-6893.2024.31422
ZOU Y C, TAO C G, ZHEN Z Y, et al. Precision Land-ing Control Based on Direct Force for Flying-wing Car-rier-based Aircraft[J]. Acta Aeronautica et Astronautica Sinica, 1-18 [2025-06-24]. https://hkxb.buaa.edu.cn/CN/10.7527/S1000-6893.2024.31422 (in Chinese).
[16] WANG X R, KAMPEN E J V, CHU Q P. Stability Anal-ysis for Incremental Nonlinear Dynamic Inversion Con-trol[J] Journal of Guidance, Control, and Dynamics, 2019 42(5), 1116-1129.
[17] WANG X R, KAMPEN E V, CHU Q P, et al. Flexible Aircraft Gust Load Alleviation with Incremental Non-linear Dynamic Inversion[J] Journal of Guidance, Con-trol, and Dynamics, 2019 42(7), 1519-1536.
[18] WANG X R. SUN S H, KAMPEN E V, et al. Quadrotor fault tolerant incremental sliding mode control driven by sliding mode disturbance observers[J]. Aerospace Science and Technology, 2019 87, 417-430.
[19] LI Y, LIU K, WEN C Y, et al. Fast fixed-time incremen-tal backstepping fault-tolerant control for aircraft with asymmetric wing damage[J]. Aerospace Science and Technology, 2025, 164, 110405.
[20] LIU K, WANG Y, LI Y, et al. Velocity-Free Adaptive Neural-Fuzzy Predefined-Time Attitude Control for Spacecraft[J]. IEEE Transactions on Aerospace and Electronic Sys-tems, 2025, 61(3): 6354-6372.
[21] WU C H, YAN J G, SHEN J H, et al. Predefined-time attitude stabilization of receiver aircraft in aerial refuel-ing[J]. IEEE Transactions on Circuits and Systems II: Express Briefs,2021, 68(10): 3321-3325.
[22] WANG Y X, WANG H L, LIU Y H, et al. Modeling and predefined-time anti-disturbance control for the aerial refueling phase of receiver aircraft[J]. Applied Mathe-matical Modelling, 2022, 112, 540-559.
[23] YU X, LIU Z X, ZHANG Y M. Fault-Tolerant Flight Control Design With Finite-Time Adaptation Under Ac-tuator Stuck Failures[J]. IEEE Transactions on Control Systems Technology, 2017, 25(4), 1431-1440.
[24] LI Y, WANG T Q, WEN C Y et al. Predefined-Time Active Fault-Tolerant Control of Transport Aircraft Subject to Control Surface Failures[J]. IEEE Transac-tions on Aerospace and Electronic Systems, 2025, 61(3): 5731-5744.
[25] LIU K, YANG W Y, YUAN Z P et al. Fast Fixed-Time Distributed Neural Formation Control-based Dis-turbance Observer for Multiple Quadrotor UAVs Under Unknown Disturbances[J]. IEEE Transactions on Aero-space and Electronic Systems, 2025, 1-17.
[26] 吴慈航, 闫建国, 钱先云, 等. 受油机指定时间姿态稳定控制[J]. 航空学报, 2022, 43(2): 324996.
WU C H, YAN J G, QIAN X Y, et al. Predefined-time at-titude stabilization control of receiver aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2022, 43(2): 324996 (in Chinese).
[27] SMEUR E J J, CHU Q P, CROON G C H E. Adaptive incremental nonlinear dynamic inversion for attitude control of micro air vehicles[J], Journal of Guidance, Control, and Dynamics, 2016, 39(3), 450-461.

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主管单位：中国科学技术协会主办单位：中国航空学会北京航空航天大学

不对称机翼损伤飞机特性分析与增量容错控制（先进飞行器安全控制专栏）

Analysis of aircraft characteristics with asymmetric wing damage and incremental fault-tolerant control

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