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基于扰动补偿MPC的直接升力着舰控制

潘子双 郁大照 韩维 崔凯凯 汪节 万兵

航空学报2026,Vol.47Issue(11):304-321,18.
航空学报2026,Vol.47Issue(11):304-321,18.DOI:10.7527/S1000-6893.2025.32810

基于扰动补偿MPC的直接升力着舰控制

Direct lift carrier landing control based on disturbance compensation MPC

潘子双 1郁大照 1韩维 1崔凯凯 2汪节 3万兵4

作者信息

  • 1. 海军航空大学 航空基础学院,烟台 264001
  • 2. 中国人民解放军92942部队,北京 100161
  • 3. 中国人民解放军91475部队,葫芦岛 125100
  • 4. 海军航空大学 岸防兵学院,烟台 264001
  • 折叠

摘要

Abstract

To address the challenges faced by carrier-based aircraft during the final landing phase,such as severe time-varying disturbances from air wake and deck motion,as well as the stringent Angle of Attack(AOA)stability re-quirement for Direct Lift Control(DLC),this paper proposes a DLC landing control framework based on disturbance-compensating Model Predictive Control(MPC).Firstly,to provide the controller with accurate state and command in-formation,a smooth and continuous landing guidance trajectory is generated based on deck motion prediction;a high-order state and disturbance observer is designed to achieve simultaneous,high-precision estimation of the aircraft's states and external disturbances.Secondly,a dual-channel framework,consisting of a"one-step"disturbance predic-tion embedded within the MPC and an AOA-prioritized adaptive feedforward compensator,is developed to achieve pri-oritized AOA stabilization and precise trajectory tracking.Finally,the effectiveness and superiority of the proposed method are validated through comparative simulations under various sea states.The results demonstrate that the pro-posed framework can achieve excellent AOA stability and high-precision trajectory tracking performance in the pres-ence of strong disturbances.

关键词

着舰控制/直接升力控制/模型预测控制/扰动补偿/鲁棒控制

Key words

carrier landing control/direct lift control/Model Predictive Control(MPC)/disturbance compensation/robust control

分类

航空航天

引用本文复制引用

潘子双,郁大照,韩维,崔凯凯,汪节,万兵..基于扰动补偿MPC的直接升力着舰控制[J].航空学报,2026,47(11):304-321,18.

航空学报

1000-6893

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