期刊文献+

基于BSP-ANN的四旋翼无人机轨迹跟踪方法 被引量:23

Trajectory tracking method for quadrotor UAV based on BSP-ANN
原文传递
导出
摘要 为了降低无人机轨迹跟踪误差,提高系统抗干扰能力,对反步(Backstepping)法进行改进提出一种基于反步神经网络(BSP-ANN)的无人机轨迹跟踪方法。首先,建立了四旋翼无人机运动学模型;然后,结合Backstepping方法在无人机的姿态控制、轨迹跟踪控制系统中引入Sigma-Pi神经网络,同时设计Sigma-Pi神经网络控制率,并证明该控制率满足Lyapunov意义下的系统稳定;最后,分别给出了相应的仿真实验。仿真结果表明:该算法可以有效降低跟踪误差,缩短无人机跟踪时间,同时可以提高系统的抗干扰能力。 To reduce the trajectory tracking error of the UAV and improve the anti-jamming ability of the system,a new trajectory tracking algorithm of the UAV is proposed based on BSP-ANN.A dynamic model for the Quadrotor UAV is given.Based on the Backstepping method,the Sigma-Pi ANN is introduced into the position control system and attitude control system of the Quadrotor UAV.The Sigma-Pi ANN control law is designed,and proving the systems stability in the sense of Lyapunov function.The corresponding simulations are performed using MATLAB.Simulation results show that with the BSP-ANN method,the trajectory tracking performance of the UAV can be improved by reducing the trajectory tracking error,decreasing the tracking time,and improving the anti-interference ability of the system.
作者 陈志明 牛康 李磊 吴云华 华冰 CHEN Zhiming;NIU Kang;LI Lei;WU Yunhua;HUA Bing(Micro Satellite Research Center, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China)
出处 《航空学报》 EI CAS CSCD 北大核心 2018年第6期177-184,共8页 Acta Aeronautica et Astronautica Sinica
基金 国家自然科学基金(61673212) 航空科学基金(20150852013) 江苏省自然科学基金(BK20161490) 上海市优秀学科带头人计划(14XD1423300)~~
关键词 无人机 轨迹跟踪 Sigma-Pi 反步神经网络 反步 UAV trajectory tracking Sigma-Pi BSP-ANN backstepping
  • 相关文献

参考文献5

二级参考文献48

  • 1苏永华,何满潮,赵明华,刘晓明.基于区间变量的响应面可靠性分析方法[J].岩土工程学报,2005,27(12):1408-1413. 被引量:21
  • 2申涛,王孝红,袁铸钢.一类不确定系统的鲁棒稳定性分析[J].自动化学报,2007,33(4):426-427. 被引量:10
  • 3Elham Semsar. Adaptive formation control of UAVsin the presence of unknown vortex forces and leaderconunands[C]. Proc of the 2006 American Control ConfMinneapolis. Minnesota: IEEE, 2006: 3563-3569.
  • 4Boskovic J D, Li S M, Mehra R K. Semi-globally stableformation flight control design in three dimensions[C].Proc of the 40th IEEE Conf on Decision and Control.Orlando: IEEE, 2001’2: 1059-1064.
  • 5Li Sai-ming, Jovan D Boskovic, Raman K Mehra.Globally stable automatic formation flight control in twodimensions[C]. AIAA Guidance, Navigation and ControlConf and Exhibit. Montreal: AIAA, 2001: 176-182.
  • 6Gaizi D. Closed-coupled formation flight control usingquasi-continuous high-qrder sliding-mode[C]. Proc of the2007 American Control Conf Marriott. New York: IEEE,2007: 1799-1804.
  • 7Fabrizio Giulietti, Lorenzo Pollini,Mario Innocenti.Autonomous formation flight[J]. IEEE Control SystemsMagazine, 2000, 25( 11): 34-45.
  • 8Bangash Z, Sanchez R, Ahmed A, et al. Aerodynamics offormation flight[C]. The 42nd AIAA Aerospace Sciences. Meeting and Exhibit. Reno: AIAA, 2004: 725.
  • 9Selcuk Bayraktar, Fainekos Georgios E, Pappas GeorgeJ. Hybird modeling and experimental cooperative controlof multiple unmanned aerial vehicles [R]. Pennsylvania:University of Pennsylvania, MS-CIS-04-32, 2004.
  • 10朱战霞,郑莉莉.无人机编队飞行控制器设计[J].飞行力学,2007,25(4):22-24. 被引量:21

共引文献98

同被引文献240

引证文献23

二级引证文献155

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部