[1] 李广华, 张洪波,汤国建.高超声速滑翔飞行器典型弹道特性分析[J].宇航学报,2015,36(4):397-403.LI G H,ZHANG H B,TANG G J.Typical trajectory characteristics of hypersonic glide vehicle[J].Journal of Astronautics,2015,36(4):397-403(in Chinese). [2] 穆凌霞, 王新民,谢蓉,等.高超音速飞行器及其制导控制技术综述[J].哈尔滨工业大学学报,2019,51(3):1-14.MU L X,WANG X M,XIE R,et al.A survey of the hypersonic flight vehicle and its guidance and control technology[J].Journal of Harbin Institute of Technology,2019,51(3):1-14(in Chinese). [3] 张灿, 林旭斌,胡冬冬,等.2018年国外高超声速飞行器技术发展综述[J].飞航导弹,2019(2):1-5.ZHANG C,LIN X B,HU D D,et al.A survey of foreign hypersonic vehicle technology development in 2018[J].Aerodynamic Missile Journal,2019(2):1-5(in Chinese). [4] 张远龙, 谢愈.滑翔飞行器弹道规划与制导方法综述[J].航空学报,2020,41(1):50-62.ZHANG Y L,XIE Y.Review of trajectory planning and guidance methods for gliding vehicles[J].Acta Aeronautica et Astronautica Sinica,2020,41(1):50-62(in Chinese). [5] BARBARINO S,BILGEN O,AJAJ R M,et al.A review of morphing aircraft[J].Journal of Intelligent Material Systems and Structures,2011,22(9):823-877. [6] VALASEK J,DOEBBLER J,TANDALE M D,et al.Improved adaptive-reinforcement learning control for morphing unmanned air vehicles[J].IEEE Transactions on Systems,Man,and Cybernetics.Part B:Cybernetics,2008,38(4):1014-1020. [7] 郭建国, 吴林旭,周军.非对称变翼飞行器复合控制系统设计[J].宇航学报,2018,39(1):52-59.GUO J G,WU L X,ZHOU J.Compound control system design for asymmetric morphing-wing aircraft[J].Journal of Astronautics,2018,39(1):52-59(in Chinese). [8] WICKENHEISER A,GARCIA E.Perching aerodynamics and trajectory optimization[C]//Active and Passive Smart Structures and Integrated System 2007.Bellingham:SPIE,2007,6525:1-9. [9] MIR I,MAQSOOD A,EISA S A,et al.Optimal morphing-augmented dynamic soaring maneuvers for unmanned air vehicle capable of span and sweep morphologies[J].Aerospace Science and Technology,2018,79:17-36. [10] 彭悟宇, 杨涛,涂建秋,等.高超声速变形飞行器翼面变形模式分析[J].国防科技大学学报,2018,40(3):15-21.PENG W Y,YANG T,TU J Q,et al.Analysis on wing deformation modes of hypersonic morphing aircraft[J].Journal of National University of Defense Technology,2018,40(3):15-21(in Chinese). [11] 彭悟宇, 杨涛,王常悦,等.高超声速伸缩翼变形飞行器轨迹多目标优化[J].国防科技大学学报,2019,41(1):41-47.PENG W Y,YANG T,WANG C Y,et al.Trajectory multi-objective optimization for hypersonic telescopic wing morphing aircraft[J].Journal of National University of Defense Technology,2019,41(1):41-47(in Chinese). [12] 陈铁彪, 龚旻,王洪波,等.临近空间可变形滑翔飞行器轨迹优化与性能分析[J].宇航学报,2018,39(9):944-952.CHEN T B,GONG M,WANG H B,et al.Trajectory optimization and performance analysis of the near-space morphing glide vehicles[J].Journal of Astronautics,2018,39(9):944-952(in Chinese). [13] BAO C Y,WANG P,TANG G J.Integrated guidance and control for hypersonic morphing missile based on variable span auxiliary control[J].International Journal of Aerospace Engineering,2019,2019:1-20. [14] 储培, 倪昆,程林,等.基于反步滑模的高超声速变体飞行器鲁棒控制[J].计算机仿真,2018,35(8):41-45.CHU P,NI K,CHENG L,et al.Robust control of hypersonic morphing vehicle based on backstepping sliding mode control[J].Computer Simulation,2018,35(8):41-45(in Chinese). [15] SHEN Z J,LU P.Onboard generation of three-dimensional constrained entry trajectories[J].Journal of Guidance,Control,and Dynamics,2003,26(1):111-121. [16] 王肖, 唐胜景,祁帅,等.带终端高度约束的再入预测校正制导[J].战术导弹技术,2018(4):70-77.WANG X,TANG S J,QI S,et al.Predictor-corrector entry guidance with terminal altitude constraint[J].Tactical Missile Technology,2018(4):70-77(in Chinese). [17] 徐瑞民. 二元非线性方程组求根的牛顿迭代法[J].山东轻工业学院学报(自然科学版),2009,23(4):89-91.XU R M.Newton's method for the nonlinear function of two independent variables[J].Journal of Shandong Institute of Light Industry(Natural Science Edition),2009,23(4):89-91(in Chinese). [18] XUE S B,LU P.Constrained predictor-corrector entry guidance[J].Journal of Guidance,Control,and Dynamics,2010,33(4):1273-1281. |