无人机自主着陆纵向控制律设计
[1] 宋辉. 复杂条件下无人机自动着陆控制技术研究[D]. 南京: 南京航空航天大学, 2011.
SONG H.Research on automatic landing control technologies for UAV under complex conditions [D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2011.(in Chinese)
[2] 车军, 张新国.自动着陆精确轨迹跟踪控制[J].北京航空航天大学学报, 2005, 9(31): 975-979.
CHE J, ZHANG X G. Exact trajectory tracking control of automatic landing [J]. Journal of Beijing University of Aeronautics and Astronautics, 2005, 9(31): 975-979.(in Chinese)
[3] 张建宏, 张平.无人机自主精确着陆控制律设计及仿真研究[J].系统仿真学报, 2009, 21(3): 743-748.
ZHANG J H, ZHANG P. Autonomous precise landing control law for UAV [J].Journal of System Simulation, 2009, 21(3): 743-748.(in Chinese)
[4] AGUSTIN G M, RODOLFO E, HABER G. Internal mode control based on neuro fuzzy system for network application [J].IEEE Transactions on Automatics Science and Engineering, 2009, 6(2): 367-372.
[5] 郭艳艳, 陈澜, 杨常伟. 无人机着陆抗风鲁棒H∞控制器设计研究[J]. 计算机测量与控制, 2010, 21(2): 348-350.
GUO Y Y, CHEN L, YANG CH W. Design of a robust H∞ controller for UAV automatic landing under wind shear [J]. Computer Measurement &Control, 2010, 21(2): 348-350.(in Chinese)
[6] JIAQ L, WANG X M. Design of a robust H∞ controller for automatic landing system of an aircraft [J]. Flight Dynamics, 2003, 21(1): 32-35.
[7] SIEBERLING S, CHU Q P, MULDER J A. Robust flight control using incremental nonlinear dynamic inversion and angular acceleration prediction [J]. Journal of Guidance, Control and Dynamics, 2010, 33(6): 1732-1742.
[8] 陈华坤, 章卫国, 王新民. 舰载机纵向自动着舰控制系统设计[J]. 弹箭与制导学报, 2007, 27(1): 73-77.
CHEN H K, ZHANG W G, WANG X M. Design of automatic control system for longitudian landing on carrier [J].Journal of projectiles, rockets, missiles and guidance, 2007, 27(1): 73-77.(in Chinese)
[9] 段镇, 高九州. 无人机滑跑线性化建模与增益调节纠偏控制[J]. 光学 精密工程, 2014, 22(6): 1507-1516.
[10] 李迪, 陈向坚, 续志军. 增益自适应滑模控制器在微型飞行器飞行姿态控制中的应用[J].光学 精密工程, 2013, 21(5): 1183-1192.
[11] 王洋, 张京娟. 基于自适应控制的无人机飞行控制系统研究[J]. 弹箭与制导学报, 2010, 30(4): 15-19.
WANG Y, ZHANG J J. Research on flight control system based adaptive controller for UAV [J].Journal of Projectiles, Rockets, Missiles and Guidance, 2010, 30(4): 15-19.(in Chinese)
[12] ALCANTARA S, PEDRET C, VILANOVA R, et al.. Generalized internal model control for balancing input/output disturbance response [J]. Ind Eng Chem Res., 2011, 50(19): 70-80.
[13] 蔡红明, 昂海松, 郑祥明. 基于自适应逆的微型飞行器飞行控制系统[J]. 南京航天航空大学学报, 2011, 43(2): 137-142.
CAI H M, ANG H S, ZHENG X M. Flight control system of MAV based on adaptive dynamic inversion [J]. Journal of Nanjing University of Aeronautics and Astronautics, 2011, 43(2): 137-142.(in Chinese)
[14] 李艳辉, 历明, 周凌. 基于模型匹配的光电侦查无人机飞行控制器设计方法[J]. 红外与激光工程, 2015, 44(2): 693-670.
[15] 吴德伟, 胡奕明. 无人机自主着陆半实物仿真系统设计[J]. 系统仿真学报, 2008, 20(24): 6815-6820.
WU D W, HU Y M. Design of hardware-in-the-loop simulation system to UAV automatic landing guidance[J]. Journal of Simulation, 2008, 20(24): 6815-6820.(in Chinese)
高九州, 贾宏光. 无人机自主着陆纵向控制律设计[J]. 光学 精密工程, 2016, 24(7): 1799. GAO Jiu-zhou, JIA Hong-guang. Design of longitudinal control law for small fixed-wing UAV during auto landing[J]. Optics and Precision Engineering, 2016, 24(7): 1799.