[1] 张智,朱契丹,张雯.航母舰载机全自动引导着舰技术[M].哈尔滨:哈尔滨工程大学出版社,2016:3-4.ZHANG Z,ZHU Q D,ZHANG W.Aircraft carrier automatic carrier landing technology[M].Harbin:Harbin Engineering University Press,2016:3-4(in Chinese). [2] 朱丽红.带有时变惯性阵无人艇的路径跟踪[D].哈尔滨:哈尔滨工程大学,2018:4-6.ZHU L H.Path following with time-varying inertial array unmanned boat[M].Harbin:Harbin Engineering University,2018:4-6(in Chinese). [3] PARK S,DEYST J,HOW J.A new nonlinear guidance logic for trajectory tracking:AIAA-2004-4900[R].Reston:AIAA,2004. [4] SAFWAT E,ZHANG W,WU M,et al.Robust path following controller for unmanned aerial vehicle based on carrot chasing guidance law using dynamic inversion[C]//The 18th International Conference on Control,Automation and System.Piscataway:IEEE Press,2018:1444-1450. [5] 马振宇,祝小平,周洲,等.全翼布局无人机滑跑轨迹跟踪方法对比与试验[J].飞行力学,2019,37(6):72-78.MA Z Y,ZHU X P,ZHOU Z,et al.Comparison and test of running path following methods for full-wing UAV[J].Flight Dynamics,2019,37(6):72-78(in Chinese). [6] ZHENG Z W,SUN L,XIE L H.Error-constrained LOS path following of a surface vessel with actuator saturation and faults[J].IEEE Transactions on Systems,Man,and Cybernetics:Systems,2018:48(10):2168-2216. [7] 李英杰,吴文海,韩维元.基于线性矩阵不等式的舰载机纵向着舰H∞控制[J].飞行力学,2005,23(3):48-51.LI Y J,WU W H,HAN W Y.H∞ control of the longitudinal carrier landing system for carrier aircraft based on LMI[J].Flight Dynamics,2005,23(3):48-51(in Chinese). [8] 邵敏敏,龚华军,甄子洋,等.基于H2预见控制的舰载机自动着舰控制方法[J].电光与控制,2015,22(9):68-71.SHAO M M,GONG H J,ZHEN Z Y,et al.An H2 preview based antomatic landing control method for carrier based aircraft[J].Electronics Optics & Control,2015,22(9):68-71(in Chinese). [9] 甄子洋,陶钢,江驹,等.无人机自动撞网着舰轨迹自适应跟踪控制[J].哈尔滨工程大学学报,2017,38(12):1922-1927. ZHEN Z Y,TAO G,JIANG J,et al.Adaptive tracking control of automatic net landing trajectory for carrier-based unmanned aerial vehicle[J].Jouurnal of Harbin Engineering University,2017,38(12):1922-1927(in Chinese). [10] ZHEN Z Y,JIANG S Y,JIANG J.Preview control and particle filtering for automatic carrier landing[J].IEEE Transactions on Aerospace and Electronic Systems,2018,54(6):2662-2674. [11] ZHEN Z Y,YU C J,JIANG S J,et al.Adaptive Super-Twisting control for automatic carrier landing of aircraft[J].IEEE Transactions on Aerospace and Electronic Systems,2020,56(2):984-997. [12] YURI A K,DEHECTOR G M,ANTON V P,et al.Guiding vector field algorithm for a moving path following problem[J].IFAC PapersOnLine,2017,50(1):6983-6988. [13] WANG Y Z,WANG D W,ZHU S Q.Cooperative moving path following for multiple fixed-wing unmanned aerial vehicles with speed constraints[J].Automatica,2019,100:82-89. [14] OLIVEIRA T,AGUIAR A P,ENCARNACAO P.Moving path following for unmanned aerial vehicles with applications to single and multiple target tracking problems[J].IEEE Transactions on Robotics,2016,32(5):1062-1078. [15] 张超,张胜修,刘毅男,等.约束自适应反步法及其在飞行控制中的应用[J].控制工程,2014,21(3):430-435.ZHANG C,ZHANG S X,LIU Y N,et al.Constrained adaptive backstepping with application to flight control[J].Control Engineering of China,2014,21(3):430-435(in Chinese). [16] 吴文海,张杨,胡云安,等.舰载机着舰非线性反演控制方法研究进展[J].系统工程与电子技术,2018,40(7):1578-1587. WU W H,ZHANG Y,HU Y A,et al.Research development in nonlinear backstepping control method of carrier-based aircraft landing[J].Systems Engineering and Electronics,2018,40(7):1578-1587(in Chinese). [17] AN H,LIU J,WANG C,et al.Approximate backstepping fault-tolerant control of the flexible air-breathing hypersonic vehicle[J].IEEE/ASME Transactions Mechatronics,2016,21(3):1680-1691. [18] 杨晓骞.不确定条件下高超声速飞行器轨迹优化与控制方法研究[D].长沙:国防科学技术大学,2016:58-59.YANG X Q.Research on trajectory optimization and control approach for hypersonic vehicle under uncertainty[D].Changsha:National University of Defense Technology,2016:58-59(in Chinese). [19] XIANG W B,XIAO Y W,RUI Z,et al.Tracking differentiator design for the robust backstepping control of a flexible air-breathing hypersonic vehicle[J].Journal of the Franklin Institute,2015,352(4):1739-1765. [20] ADAMS R J,BUFFINGTON J M,BANDA S S.Design of nonlinear control laws for high-angle-of-attack flight[J].Journal of Guidance,Control, and Dynamics,2012,17(4):737-746. [21] CHAKRABORY A,SEILER P,BALAS G J.Susceptibility of F/A-18 flight controllers to the falling-leaf mode:Linear analysis[J].Journal of Guidance,Control,and Dynamics,2011,34(1):73-85. [22] 徐倩,王肖,吴洁,等.基于扩张状态观测器和指令滤波器的导弹姿态控制[J].飞行力学,2018,36(1):52-55.XV Q,WANG X,WU J,et al.Attitude control of missile based on extended state observer and command filter[J].Flight Dynamics,2018,36(1):52-55(in Chinese). [23] 甄子洋,王新华,江驹,等.舰载机自动着舰引导与控制研究进展[J].航空学报,2017,38(2):127-148.ZHEN Z Y,WANG X H,JIANG J,et al.Research progress in guidance and control of automatic carrier landing of carrier-based aircraft[J].Acta Aeronautica et Astronautica Sinica,2017,38(2):127-148(in Chinese). [24] 张志冰,甄子洋,江驹,等.舰载机自动着舰引导与控制综述[J].南京航空航天大学学报,2018,50(6):734-744.ZHANG Z B,ZHEN Z Y,JIANG J,et al.Review on development in guidance and control of automatic carrier landing of carrier-based aircraft[J].Journal of Nanjing University of Aeronautics & Astronautics,2018,50(6):734-744(in Chinese). [25] NAPOLITANO M,PARIS A,SEANOR B,et al.Estimation of the longitudinal aerodynamic parameters from flight data for the NASA F/A-18 HARV[C].Proceedings of the 21st Atmospheric Flight Mechanics Conference,2013:469-478. |