期刊文献+

某小型无人机导航控制算法研究 被引量:2

Investigation of the Navigation and Control Algorithm for a Small UAV
下载PDF
导出
摘要 研究了可实现小型无人机自主飞行的控制、导航算法。建立了描述无人机运动的状态空间模型,在此基础上分析了开环系统对扰动的响应。针对响应结果,采用最优控制理论设计了带有全维状态观测器的控制器;使用了基于李雅普诺夫向量场的导航算法并对控制器和导航算法进行仿真。研究结果表明,文中给出的控制和导航算法具有良好的性能指标,可跟踪任意航路点,从而可以实现无人机自主飞行。 The navigation and control methods which can achieve autonomous flight for UAV were investigated in this paper. The state space model of the UAV was established. The response to disturbance of the open-loop system was analyzed. A lateral direction autopilot with state observer was designed by using LQR method. Then, a navigation algorithm named Lyapunov vector field was presented. The navigation and control strategies were both simulated in time domain. The results illuminate the proposed methodologies have satisfying performance and can track arbitrary waypoint. Consequently, requirement of automatic flight was achieved.
作者 李蒙 刘莉
出处 《弹箭与制导学报》 CSCD 北大核心 2011年第1期37-40,44,共5页 Journal of Projectiles,Rockets,Missiles and Guidance
关键词 无人机 飞行控制 导航 状态观测器 李雅普诺夫向量场 UAV flight control navigation state observer Lyapunov vector field
  • 相关文献

参考文献6

  • 1Jang J, Tomlin C. Autopilot design for the stanford Dragon Fly UAV: Validation through hardware-in-the- loop Simulation[C]//AIAA Guidance, Navigation and Control Conference, Washington, DC, 2001.
  • 2张明廉.飞行控制系统[M].北京:航空工业出版社,1994.41-45.
  • 3J Hall, K Mohseni, D Lawrence. Lateral control of a tailless micro aerial vehicle[C]//AIAA Guidance, Nav- igation, and Control Conference, Keystone, 2006.
  • 4D A Lawrence, E Frew, W Pisano. Lyapunov vector fields for autonomous UAV flight control [C]//AIAA Guidance, Navigation and Control Conference and Ex- hibit, South Carolina, 2007.
  • 5W Pisano, Dale A Lawrence, Peter C Gray. Autonomous UAV control using a 3-sensor autopilot[C]// AIAA, 2007 Conference and Exhibit, California, 2007.
  • 6H Khalil. Nonlinear systems[M]. 3rd ed. Beijing: Publishing House of Electronics Industry,2007.

共引文献115

同被引文献24

  • 1谭述森.北斗卫星导航系统的发展与思考[J].宇航学报,2008,29(2):391-396. 被引量:179
  • 2范胜林,胡国辉,林雪原,袁信.GPS定位定向系统的研制[J].仪器仪表学报,2004,25(6):820-824. 被引量:15
  • 3何炬.国外天文导航技术发展综述[J].舰船科学技术,2005,27(5):91-96. 被引量:49
  • 4苏宛新 张志敏 黄春梅等.GPS/INS组合导航系统设计方法研究.电子测量与仪器学报,2006,20:545-549.
  • 5RUANGWISET, A. Path generation for ground target tracking of airplane-typed UAV [ C ]. Robotics and Bio- mimetics, Bangkok, Thailand, 2009: 1354-1358.
  • 6CONTE G, DOHERTY P. An integrated UAV navigation system based on aerial image matching[ C]. IEEE Aero- snace Conference. 2008.1-10.
  • 7RAIMONDI F M, MELLUSO M. Stability and noises evaluation of Fuzzy/Kalman UAV navigation system [ C ]. Decision and Control, China, 2009:768-775.
  • 8WHITMORE S A, MOES T R. Design of a flush airdata system (FADS) for the hypersonic air launched option (HALO) vehicle [ R ]. NASA Dryden Flight Research Center, 2001.
  • 9DENTI E, GALATOLO R, SCHETFINI F. Aircraft state estimation : Inertial and air data systems [ C ]. 2nd Euro- pean Conference for Aero-Space Sciences, 2007.
  • 10叶卫东,熊鹏.分布式大气数据计算机综合测试系统设计[J].微计算机信息,2008,24(31):72-74. 被引量:4

引证文献2

二级引证文献22

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