| [1] 卜祥伟. 高超声速飞行器飞行控制研究进展[J]. 航空兵器, 2018(01): 47-61. [2] MA X B, DING Y B, YUE X K. Optimal adaptive finite-time control for flexible near-space vehicle based on Deep Forest[J]. Advanced Engineering Informatics, 2026, 69(pa):103892.[3] 张希彬,宗群,曾凡琳,等.考虑气动—推进—弹性耦合的高超声速飞行器面向控制建模与分析[J].宇航学报, 2014, 35(5):528-536.[4] 叶正寅,孟宪宗,刘成,等.高超声速飞行器气动弹性的近期进展与发展展望[J].空气动力学学报, 2018.[5] 褚凯佟,张伦,邱云龙,等.壁面滑移与气体引射对平板边界层稳定性的耦合影响[J].物理学报, 2026, 75(11).DOI:10.7498/aps.75.20260062.[6] Tao R, Ding Y, Li H, et al. Dual-channel event-triggered practical predefined-time formation controller for multi space transport robot system[J].Aerospace Science and Technology, 2025, 159(000). DOI: 10.1016/j.ast.2025.109976.[7] HUANG S T, JIANG J, LI O X. Sliding mode backstepping control for the ascent phase of near-space hypersonic vehicle based on a novel triple power reaching law[J]. Aerospace, 2022, 9(12): 755.[8] GUO R Y, DING Y B, YUE X K. Active adaptive continuous nonsingular terminal sliding mode controller for hypersonic vehicle[J]. Aerospace Science and Technology, 2023, 137: 108279.[9] TANG X N, ZHAI D, LI X J. Adaptive fault-tolerance control based finite-time backstepping for hypersonic flight vehicle with full state constrains[J]. Information Sciences, 2020, 507: 53-66.[10] 李娜英,岳晓奎,丁一波,等.深度森林算法在高速飞行器智能控制中的应用研究[J].宇航学报,2025,46(11):2277-2290.[11] 王鹏飞,蒋坤,张峰.高超声速飞行器输入受限反步控制[J].战术导弹技术,2023,(2):57-65.[12] 胡超芳,刘欣悦.弹性高超声速飞行器分解式输出反馈预测控制[J].天津大学学报(自然科学与工程技术版), 2025, 58(12):1230-1241.[13] ZHANG T C, DING Y B, YUE X K, et al. Adaptive terminal super-twisting prescribed performance controller for near-space vehicle based on data-driven model[J]. ISA Transactions, 2025, 160(000):1-18.[14] 许斌,王霞. 基于时标分解的弹性高超声速飞行器智能控制[J]. 航空学报,2020,41(11):26-35.[15] Piao M N, Yang Z H, Sun M W, et al. Synthesis of attitude control for statically unstable hypersonic vehicle with low-frequency aero-servo-elastic effect[J]. Aerospace Science and Technology, 2018, 80(SEP.):67-77.[16] 陈尔康.弹性高超声速飞行器的状态/参数估计与分层滑模控制[D].哈尔滨工业大学,2020.[17] 王青,张伸,梁津津,等.降低频带耦合的强静不稳定弹性飞行器控制[J].弹箭与制导学报, 2017, 37(6):5.[18] 樊朋飞,凡永华,于云峰.高超声速飞行器伺服弹性与静不稳定控制方法[J].战术导弹技术, 2016(2):7.[19] 许志,马宗占,唐硕.一种高超声速试飞器助推段主动弹性抑制方法[J].宇航学报, 2019, 40(10):9.[20] PU Z Q, YUAN R Y, TAN X M, et al. Active robust control of uncertainty and flexibility suppression for air-breathing hypersonic vehicles[J]. Aerospace Science and Technology, 2015, 42: 429-441.[21] WANG X, XU B. Robust adaptive control of hypersonic flight vehicle with aero-servo-elastic effect[J]. IEEE Transactions on Aerospace and Electronic Systems, 2023, 59: 1955-1964.[22] 石永峰,代金国,祝玉东.弹性高超声速飞行器振动抑制的自适应控制方法[J].飞行力学, 2019, 37(6):5.[23] 朴敏楠、陈志刚、孙明玮、陈增强.高超声速飞行器气动伺服弹性的自适应抑制[J].航空学报, 2020, 41(11):15.[24] 蒲利东,罗务揆,严泽洲.气动伺服弹性系统结构陷幅滤波器优化设计[J].工程力学, 2018, 35(4):235-241.[25] SIGTHORSSON D O, SERRANI A. Development of linear parameter-varying models of hypersonic air-breathing vehicles[R]. 2009.[26] MOULAY E, et al. Robust fixed-time stability: application to sliding mode control[J]. IEEE Transactions on Automatic Control, 2021: 1-1.[27] SUDALAGUNTA P R, et al. Aeroelastic control-oriented modeling of an airbreathing hypersonic vehicle[J]. Journal of Guidance, Control, and Dynamics, 2018, 41: 1136-1149. |