期刊文献+

密集障碍物环境下基于凸包和微粒群优化的机器人路径规划 被引量:15

Robot path planning in environments with dense obstacles based on convex hull and particle swarm optimization
下载PDF
导出
摘要 密集障碍物环境下,考虑机器人移动过程中的控制偏差进行路径规划,尚缺乏有效的方法.本文的方法是:首先根据障碍物之间的最小距离和机器人尺寸的大小关系,确定凸包形成的条件;然后,通过选择满足条件的顶点,形成密集障碍物的凸包;最后,基于凸包的关键点和稀疏障碍物的位置,采用微粒群优化规划机器人路径.仿真和实验结果验证了所提方法的可行性. Effective methods are lacking for planning robot path while considering control deviation in an environment , : with dense obstacles. In our approach, we first determine the prerequisites for forming a convex hull according to the relation between the robot size and the minimal distance between obstacles, and then, we form the convex hull of these dense obstacles by choosing vertices that satisfy certain conditions; finally, the particle swarm optimization is applied to planning the robot path based on the positions of the key vertices in the convex hull and the positions sparse obstacles. Simulation and experiment results validate the feasibility of our method.
出处 《控制理论与应用》 EI CAS CSCD 北大核心 2012年第5期609-616,共8页 Control Theory & Applications
基金 国家自然科学基金资助项目(61005089) 江苏省自然科学基金资助项目(BK2008125)
关键词 机器人 路径规划 密集障碍物 凸包 微粒群优化 robot path planning dense obstacles convex hull particle swarm optimization
  • 相关文献

参考文献8

二级参考文献55

共引文献198

同被引文献152

  • 1张颖,吴成东,原宝龙.机器人路径规划方法综述[J].控制工程,2003,10(z1):152-155. 被引量:66
  • 2熊菁,秦子增,程文科,文红武.翼伞系统分段归航轨迹的优化设计[J].航天返回与遥感,2004,25(3):11-16. 被引量:10
  • 3熊菁,秦子增,文红武.翼伞系统归航的最优控制[J].航天控制,2004,22(6):32-36. 被引量:8
  • 4王晶,黄真.工业机器人在特殊位形下的瞬时运动[J].机器人,1997,19(4):250-255. 被引量:1
  • 5GOODRICK T E Wind effect on gliding parachute systems with non- proportional automatic homing control, AD-698549 [R]. MA, USA: Army Natick Research and Eevelopment Labs, 1969.
  • 6LI Y L, LIN H B. Theoretical investigation of gliding parachute tra- jectory with deadband and non-proportional automatic homing con- trol, AIAA-91-0834 [R]. Beijing: Chinese Academy of Space Tech- nology, 1991.
  • 7SOPPA U, STRAUCH H. GNC concept for automated landing of a large parafiol, AIAA-97-1464 [R]. St. Cloud, France: Dassault Avi- ation, 1997.
  • 8JANN T. Aerodynamic model identification and GNC design for the parafoil-load system ALEX, AIAA-2001-2015 [R]. Braunschweig, Germany: DLR, 2001.
  • 9郑成,吴庆宪,姜长生,等.基于IAGA的翼伞系统分段归航轨迹的优化[J].光电与控制,2011,18(2):69-72.
  • 10BETTS J T. Survey numerical methods for trajectory optimization [J]. Journal of Guidance, Control and Dynamics, 1998, 21(2): 192 - 207.

引证文献15

二级引证文献94

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