先进拦截飞行器直/气复合控制技术综述

史伟强; 韦国军

doi:10.7643/issn.1672-9242.2026.07.010

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装备环境工程 ›› 2026, Vol. 23 ›› Issue (7) : 97-107. DOI: 10.7643/issn.1672-9242.2026.07.010

航空航天装备

先进拦截飞行器直/气复合控制技术综述

史伟强, 韦国军

作者信息 +

Research Review on Blended Direct Force and Aerodynamic Control Technology for Advanced Interceptor Vehicles

SHI Weiqiang, WEI Guojun

Author information +

文章历史 +

摘要

系统梳理了近年来国内外直/气复合控制领域的研究成果,首先阐明了姿控式、轨控式和姿轨控式3种基本方案的构型特点与适用边界。其次分析了直接力动态特性、喷流干扰效应及弹性振动耦合等建模核心问题。随后系统梳理了从滑模控制、自抗扰控制到智能控制的控制律技术发展脉络,并结合执行机构工程约束讨论了各方法的适用场景。最后探讨了制导律匹配、控制分配策略及制导控制一体化等系统集成问题。在此基础上,总结了该领域的技术演进趋势及所面临的工程挑战。最后指出,弹性振动下控制切换与结构安全的联合约束、智能策略在末端拦截中的安全性验证,以及多弹协同中单弹剩余能力与群体决策的实时衔接,仍是尚未充分解决的难题。

Abstract

This paper systematically reviews the research achievements in the field of blended direct force and aerodynamic control worldwide in recent years. Firstly, it clarifies the configuration characteristics and application boundaries of the three fundamental schemes: attitude control, orbit control, and attitude-orbit integrated control. Secondly, it analyzes the core modeling issues including direct force dynamic characteristics, jet interaction effects, and elastic vibration coupling. Subsequently, it systematically traces the technological evolution of control law methodologies from sliding mode control (SMC) and active disturbance rejection control (ADRC) to intelligent control, and discusses the applicable scenarios of each method in conjunction with actuator engineering constraints. Finally, it explores the system integration problems such as guidance law matching, control allocation strategies, and integrated guidance and control (IGC). On this basis, the technological evolution trends and engineering challenges in this field are summarized. This paper points out that the joint constraints of control switching and structural safety under elastic vibration, the safety verification of intelligent strategies in terminal interception, and the real-time integration of individual missile remaining capabilities and group decision-making in multi-interceptor cooperation remain inadequately addressed challenges.

导出引用

史伟强, 韦国军. 先进拦截飞行器直/气复合控制技术综述[J]. 装备环境工程. 2026, 23(7): 97-107 https://doi.org/10.7643/issn.1672-9242.2026.07.010

SHI Weiqiang, WEI Guojun. Research Review on Blended Direct Force and Aerodynamic Control Technology for Advanced Interceptor Vehicles[J]. Equipment Environmental Engineering. 2026, 23(7): 97-107 https://doi.org/10.7643/issn.1672-9242.2026.07.010

中图分类号： TJ765

参考文献

[1] 赵良玉, 雍恩米, 王波兰. 反临近空间高超声速飞行器若干研究进展[J]. 宇航学报, 2020, 41(10): 1239-1250.
ZHAO L Y, YONG E M, WANG B L.Some Achievements on Interception of near Space Hypersonic Vehicles[J]. Journal of Astronautics, 2020, 41(10): 1239-1250.
[2] 魏明英. 直接侧向力与气动力复合控制技术综述[J]. 现代防御技术, 2012, 40(1): 52-54.
WEI M Y.Summary of Blended Control Technology for Missiles with Lateral Jets and Aerodynamic Surfaces[J]. Modern Defence Technology, 2012, 40(1): 52-54.
[3] 魏明英. 远程防空导弹飞行控制方法研究[M]. 北京: 中国宇航出版社, 2022.
WEI M Y.Research on Flight Control Method of Long-Range Air Defense Missile[M]. Beijing: China Astronautic Publishing House, 2022.
[4] 刘凯. 导弹直/气复合控制系统的自适应控制[D]. 洛阳: 河南科技大学, 2018.
LIU K.Adaptive Control of Missile Direct/Air Composite Control System[D]. Luoyang: Henan University of Science and Technology, 2018.
[5] 李陟, 魏明英, 周荻, 等. 防空导弹直接侧向力/气动力复合控制技术[M]. 北京: 中国宇航出版社, 2012.
LI Z, WEI M Y, ZHOU D, et al.Direct Lateral Force/Aerodynamic Compound Control Technology for Air Defense Missiles[M]. Beijing: China Astronautic Publishing House, 2012.
[6] 孙兴龙, 付主木, 宋书中. 轨控式直/气复合控制导弹过载指令动态分配设计[J]. 信息与控制, 2018, 47(5): 627-633.
SUN X L, FU Z M, SONG S Z.Design of Dynamic Allocation of Overload Command for Orbital Blended Control Missile with Thrust and Aerodynamics[J]. Information and Control, 2018, 47(5): 627-633.
[7] 郭建国, 彭谦, 周敏. 直接力/气动力复合控制技术发展综述[J]. 航空兵器, 2022, 29(1): 1-13.
GUO J G, PENG Q, ZHOU M.Review on Development of Direct Force/Aerodynamic Force Compound Control Technology[J]. Aero Weaponry, 2022, 29(1): 1-13.
[8] SANAKA S P, SHARMA R K, RAMANA MURTY G V, et al. Re-Entry Vehicle Performance Analysis under the Control of Lateral Jet[J]. The Aeronautical Journal, 2024, 128(1322): 756-770.
[9] 李思远, 袁宇祺, 周荻, 等. 一种考虑模型不确定性的直/气复合飞行器无模型姿态控制方法: CN119861552B[P].2025-10-31.
LI S Y, YUAN Y Q, ZHOU D, et al. Model-Free Attitude Control Method for Direct Force/Aerodynamic Force Compound Vehicle Considering Model Uncertainty: CN119861552B[P].2025-10-31.
[10] 赵忠良, 李浩, 赖江, 等. 导弹模型直气复合气动特性研究[J]. 空天防御, 2022, 5(3): 1-9.
ZHAO Z L, LI H, LAI J, et al.Aerodynamic Characteristics of a Missile Model with Direct Force and Aerodynamic Force Compound Control Technology[J]. Air&Space DEFENSE, 2022, 5(3): 1-9.
[11] 周凤岐, 何光宇, 周军, 等. 基于直\气复合的再入飞行器操纵耦合分析及鲁椿控制设计[J]. 火力与指挥控制, 2010, 35(7): 66-69.
ZHOU F Q, HE G Y, ZHOU J, et al.Coupling Analysis and Robust Controller Design Based on Direct Force\Aerodynamic Controlled Re-Entry Aircraft[J]. Fire Control & Command Control, 2010, 35(7): 66-69.
[12] SCALLION W I.Aerodynamic Reaction Control System (RCS) Orientation and Jet Interaction (JI) Model Validation[R]. Washington: NASA Engineering and Safety Center Technical Bulletin, 2014.
[13] YANG J Y, ZENG S H, ZHAO W W, et al.Numerical Assessment of Double Lateral Jets Interaction in Rarefied Nonequilibrium Crossflows via Nonlinear Coupled Constitutive Relations[J]. Aerospace Science and Technology, 2025, 157: 109851.
[14] ZHOU K J, LOU Y C, ZHANG S Q, et al.Surrogate Multi-Objective Optimization of Missile RCS Performance in Hypersonic Rarefied Flow of the near Space[J]. AIP Advances, 2024, 14(7): 075319.
[15] ZHAO H Y, CHENG F, ZHANG Y B, et al.Numerical Study of Hot-Gas Side Jet in Supersonic Flow[C]//Proceedings of 3rd 2023 International Conference on Autonomous Unmanned Systems (3rd ICAUS 2023). Singapore: Springer, 2024.
[16] 万钊, 华如豪, 陈琦, 等. 考虑多种物理效应的轨控喷流数值计算研究[J]. 上海航天(中英文), 2025, 42(2): 194-202.
WAN Z, HUA R H, CHEN Q, et al.Numerical Simulation of Orbit-Controlled Jet Considering Multi-Physical Effects[J]. Aerospace Shanghai (Chinese & English), 2025, 42(2): 194-202.
[17] 傅杨奥骁, 刘庆宗, 丁明松, 等. 热喷干扰气体模型对飞行器气动特性影响分析[J]. 力学学报, 2022, 54(5): 1229-1241.
FU Y, LIU Q Z, DING M S, et al.Analysis of Gas Model’s Influence on Aerodynamic Characteristics for Hypersonic Vehicle over Hot Jet Interaction Flow Field[J]. Chinese Journal of Theoretical and Applied Mechanics, 2022, 54(5): 1229-1241.
[18] 周荻, 邵春涛. 大气层内拦截弹直接侧向力/气动力混合控制系统设计[J]. 宇航学报, 2007, 28(5): 1205-1209.
ZHOU D, SHAO C T.Hybrid Control System Design for an Atmospheric Interceptor Controlled by Lateral Jet Thrusters and Aerodynamic Surfaces[J]. Journal of Astronautics, 2007, 28(5): 1205-1209.
[19] IDAN M, SHIMA T, GOLAN O M.Integrated Sliding Mode Autopilot-Guidance for Dual-Control Missiles[J]. Journal of Guidance, Control, and Dynamics, 2007, 30(4): 1081-1089.
[20] SHTESSEL Y B, SHKOLNIKOV I A, LEVANT A.Guidance and Control of Missile Interceptor Using Second-Order Sliding Modes[J]. IEEE Transactions on Aerospace and Electronic Systems, 2009, 45(1): 110-124.
[21] 金一欢, 冯昊, 林俊, 等. 基于自适应高阶滑模的直气复合控制律设计[J]. 空间控制技术与应用, 2020, 46(1): 31-36.
JIN Y H, FENG H, LIN J, et al.Adaptive Continuous Higher Order Sliding Mode Control for Dual Aero/Propulsive Missile[J]. Aerospace Control and Application, 2020, 46(1): 31-36.
[22] 吕先敬, 程笠, 陈旭, 等. 基于双环滑模控制的直/气复合控制系统设计[J]. 飞控与探测, 2020, 3(5): 58-66.
LYU X J, CHENG L, CHEN X, et al.The Design of Aerodynamic/Reaction Blended Control System Based on Dual-Loop Sliding Mode Control[J]. Flight Control & Detection, 2020, 3(5): 58-66.
[23] 潘瑾瑜, 马建伟, 宋晓娜. 直接力/气动力复合控制系统的有限时间镇定[J]. 火力与指挥控制, 2016, 41(10): 75-79.
PAN J Y, MA J W, SONG X N.Finite-Time Stabilization for Lateral Jet and Aerodynamics Compound Control System[J]. Fire Control & Command Control, 2016, 41(10): 75-79.
[24] 郭超, 梁晓庚, 王俊伟, 等. 临近空间拦截弹的非奇异终端滑模控制[J]. 宇航学报, 2015, 36(1): 58-67.
GUO C, LIANG X G, WANG J W, et al.Nonsingular Terminal Slide Mode Control for near Space Interceptor[J]. Journal of Astronautics, 2015, 36(1): 58-67.
[25] 李政, 于剑桥, 赵新运. 空空导弹敏捷转弯固定时间收敛滑模控制[J]. 航空学报, 2023, 44(8): 203-216.
LI Z, YU J Q, ZHAO X Y.Fixed-Time Convergent Sliding Mode Control for Agile Turn of Air-to-Air Missiles[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(8): 203-216.
[26] LI J X, YU J Q.Fixed-Time Anti-Saturation Tracking Control for Agile Missiles with Multiple Actuators[J]. Aerospace, 2024, 11(9): 779.
[27] LI J X, YU J Q.Fixed-Time Blended Control for Agile Missiles with the Novel Multi-Source Control Mode[C]//Proceedings of 2024 International Conference on Guidance, Navigation and Control. Singapore: Springer, 2025.
[28] 毕永涛, 王宇航, 姚郁. 直/气复合控制导弹的模型预测和自抗扰姿态控制设计[J]. 宇航学报, 2015, 36(12): 1373-1383.
BI Y T, WANG Y H, YAO Y.Attitude Control Design of Missiles with Dual Control Based on Model Predictive Control and Active Disturbance Rejection Control[J]. Journal of Astronautics, 2015, 36(12): 1373-1383.
[29] 通雁辉, 陈意芬, 贾世伟. 直/气复合控制导弹的自抗扰控制系统设计研究[J]. 上海航天, 2017, 34(1): 43-50.
TONG Y H, CHEN Y F, JIA S W.Study on ADRC System Design of Missiles with Aerodynamics and Lateral Thrust[J]. Aerospace Shanghai, 2017, 34(1): 43-50.
[30] 刘凯, 杨宝庆. 一种基于自抗扰方法的姿控直气复合控制系统设计[J]. 空天防御, 2021, 4(2): 40-47.
LIU K, YANG B Q.Compound Control System Design with Lateral Thrust and Aerodynamic Force Based on ADRC Method[J]. Air & Space Defense, 2021, 4(2): 40-47.
[31] 陈光山, 车荣, 夏斌, 等. 基于最优控制/自抗扰控制的直/气复合控制系统设计研究[J]. 上海航天, 2018, 35(4): 12-17.
CHEN G S, CHE R, XIA B, et al.Study on Aerodynamic/Reaction Blended Control System Design Based on Optimal Control and Auto-Disturbance-Rejection Control[J]. Aerospace Shanghai, 2018, 35(4): 12-17.
[32] CHITSAZ A, NAGHASH A, SABERI F F.Integrated Guidance and Control Design by Active Disturbance Rejection Method for High-Velocity Target Interceptor with DCS Thruster[J]. Scientific Reports, 2024, 14: 1298.
[33] 宋晓娜, 刘凯, 宋帅. 导弹复合控制系统的神经网络控制器设计[J]. 电光与控制, 2018, 25(8): 74-77.
SONG X N, LIU K, SONG S.Neural Network Controller Design for Missile Compound Control System[J]. Electronics Optics & Control, 2018, 25(8): 74-77.
[34] 裴新月, 于勇, 李政, 等. 基于神经网络优化直/气复合控制导弹迅捷转弯[J]. 兵工学报, 2024, 45(10): 3564-3576.
PEI X Y, YU Y, LI Z, et al.Control of Quick Turning of Missile with Lateral Thrust and Aerodynamics Based on Neural Network[J]. Acta Armamentarii, 2024, 45(10): 3564-3576.
[35] 邓伟伟. 基于自适应神经模糊推理系统的导弹直/气复合控制系统设计[J]. 导航定位与授时, 2021, 8(5): : 54-60.
DENG W W.Design of Missile Direct/Air Compound Control System Based on Adaptive Neuro-Fuzzy Inference System[J]. Navigation Positioning and Timing, 2021, 8(5): : 54-60.
[36] 高晨, 马文涛, 张庆振. 基于模糊PID的直/气复合再入控制方法研究[J]. 系统仿真学报, 2010, 22(S1): 146-148.
GAO C, MA W T, ZHANG Q Z.Reaction-Jet/Aerodynamic Compound Re-Entry Control Method Research Based on Fuzzy PID Control[J]. Journal of System Simulation, 2010, 22(S1): 146-148.
[37] HE S M, SHIN H S, TSOURDOS A.Computational Missile Guidance: A Deep Reinforcement Learning Approach[J]. Journal of Aerospace Information Systems, 2021, 18(8): 571-582.
[38] 张婉滢, 司马珂, 张育禾, 等. 基于近端策略优化的多弹协同围捕机动目标制导控制方法[J]. 空天防御, 2025, 8(4): 94-103.
ZHANG W Y, SIMA K, ZHANG Y H, et al.The Guidance and Control Method of Multi-Missile Cooperative Encirclement of Maneuvering Targets Based on Proximal Policy Optimization[J]. Air&Space DEFENSE, 2025, 8(4): 94-103.
[39] WANG C F, ZHANG X Y, DONG F.Terminal Guidance Law of Missile Based on Soft Actor-Critic with Impact Angle Constraint[C]//Proceedings of 2024 43rd Chinese Control Conference (CCC). Kunming: IEEE, 2024.
[40] GIRAL F, GOMEZ I, LE CLAINCHE S.Intercepting Unauthorized Aerial Robots in Controlled Airspace Using Reinforcement Learning[J]. Aerospace Science and Technology, 2026, 168: 110985.
[41] WANG X, DENG Y F, CAI Y L, et al.Deep Recurrent Reinforcement Learning for Intercept Guidance Law under Partial Observability[J]. Applied Artificial Intelligence, 2024, 38(1): 2355023.
[42] 熊少锋, 魏明英, 赵明元, 等. 考虑导弹速度时变的角度约束最优中制导律[J]. 控制理论与应用, 2018, 35(2): 248-257.
XIONG S F, WEI M Y, ZHAO M Y, et al.Impact Angle Constrained Optimal Midcourse Guidance Law for Missiles of Time-Varying Speed[J]. Control Theory & Applications, 2018, 35(2): 248-257.
[43] 邵雷, 张金鹏, 曹有亮. 基于鲁棒轨迹跟踪的直/气复合鲁棒控制设计[J]. 航空兵器, 2016, 23(1): 35-39.
SHAO L, ZHANG J P, CAO Y L.Blended Robust Control Method with Lateral Thrust and Aerodynamic Force Based on Robust Trail Tracking[J]. Aero Weaponry, 2016, 23(1): 35-39.
[44] LIU S X, YAN B B, HUANG W, et al.Current Status and Prospects of Terminal Guidance Laws for Intercepting Hypersonic Vehicles in near Space: A Review[J]. Journal of Zhejiang University: Science A, 2023, 24(5): 387-403.
[45] CHEN W X, HU Y D, GAO C S, et al.Three-Dimensional Trajectory Tracking Guidance Against Near-Space Maneuvering Targets with Multiple Constraints under Wind Field[J]. Control Engineering Practice, 2024, 142: 105745.
[46] DOMAN D B, GAMBLE B J, NGO A D.Quantized Control Allocation of Reaction Control Jets and Aerodynamic Control Surfaces[J]. Journal of Guidance, Control, and Dynamics, 2009, 32(1): 13-24.
[47] ZHENG X, DI H J, ZHU J F.Control Allocation for Spin Interceptor with Aerodynamics and Lateral Thrust Blended[C]//Proceedings of 2023 International Conference on Advanced Unmanned Aerial Systems (ICAUS 2023). Singapore: Springer, 2024.
[48] 高振馨, 赵炜, 王一冲, 等. 基于零控脱靶量和过载偏差的直/气复合控制策略[J]. 空天防御, 2022, 5(4): 47-52.
GAO Z X, ZHAO W, WANG Y C, et al.Compound Control Strategy for Missile with Lateral Thrust and Aerodynamic Based on Zero-Effort Miss and Overload Error[J]. Air&Space DEFENSE, 2022, 5(4): 47-52.
[49] YANG Y C.Practical Optimization Method of Control Allocation for Dual-Controlled Agile Missile[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2025, 239(15): 2164-2175.
[50] JEONG I H, KIM H G.Nonlinear Autopilot for Improving Guidance Performance of Dual-Controlled Missiles with Lateral Thrust Regulation[J]. International Journal of Control, Automation and Systems, 2024, 22(12): 3559-3569.
[51] AUTENRIEB J, GRUHN P.Control Allocation Algorithm for Hypersonic Glide Vehicles with Input Limitations[C]//Porceedings of the AIAA SciTech Forum 2025. [s. l.]: AIAA, 2025.
[52] ÖZKURT S, GRIMM A, FICHTER W. Constrained Control Allocation with Continuous-Time Rate Constraints: Three-Dimensional Case[EB/OL]. (2025-07-21)[2026-05-09]. https://arxiv.org/abs/2507.15489.
[53] SONG H T, ZHANG T.Fast Robust Integrated Guidance and Control Design of Interceptors[J]. IEEE Transactions on Control Systems Technology, 2016, 24(1): 349-356.
[54] FU B, FU W X, GUO H, et al.Partial Integrated Guidance and Control Method for the Interception of Nearspace Hypersonic Target[C]//Proceedings of the 2017 13th IEEE International Conference on Control & Automation (ICCA). Ohrid: IEEE, 2017.
[55] PENG Q, CHEN G, GUO J G, et al.Attitude/Orbit Engine Compound Control for Hypersonic Target Interceptor with Discrete-Time Inputs and State Constraints[J]. IEEE Transactions on Aerospace and Electronic Systems, 2024, 60(4): 4939-4951.
[56] PENG Q, CHEN G, GUO J G, et al.Koopman Predictor-Based Integrated Guidance and Control under Multi-Force Compound Control System[J]. Aerospace, 2025, 12(3): 213.
[57] KIM H G, BECK D.Integrated Guidance and Control for Collision Course Stabilization of Dual-Controlled Interceptors[J]. Aerospace, 2024, 11(1): 9.
[58] LI J F, SONG S M, SHI X P.Full State-Constrained Integrated Guidance and Control for Aerial Interceptors with Tunnel Prescribed Performance Using Integral Barrier Lyapunov Function[J]. International Journal of Robust and Nonlinear Control, 2024, 34(12): 8090-8126.
[59] CUI L, ZHEN Z, ZHANG K, et al.Integrated Guidance and Control Based on Nonlinear Model Predictive Control with Simplified Primal-Dual Neural Network Optimization[J]. Journal of the Franklin Institute, 2024, 361(16): 107195.