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PZT在拍翅式仿昆微型飞行机器人动力系统中的应用 被引量：1

Application of PZT for insect-like flying microrobot driving system
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摘要 分析了PZT驱动和拍翅式仿昆微型飞行机器人翅运动的特点,探讨了PZT在飞行机器人驱动 系统中的应用,设计了一种具有两自由度的驱动机构,能够带动翅膀实现复杂的运动形式。 In this paper, the characteristics of PZT driver moving model of flapping wing forinsect-like flying microrobots are analyzed, and theapplications of PZT forinsect-like flying microrobots arediscussed aswell.Adriving mechanismwith twoDOFs (DegreeOfFreedom)is designed, and it can drive wing to move with complex path.
作者 周建华 王姝歆 颜景平
机构地区 东南大学机械系
出处 《制造业自动化》 北大核心 2005年第2期30-31,34,共3页 Manufacturing Automation
基金 211工程振兴行动计划(3008002102)
关键词 仿昆飞行 微型机器人 机构 PZT insect-like fly microrobot mechanism PZT
分类号 TP24 [自动化与计算机技术—检测技术与自动化装置]
  • 相关文献

参考文献6

  • 1周建华,颜景平,王姝歆,张志胜.微型仿昆飞行机器人关键技术的研究[J].机器人,2003,25(z1):751-755. 被引量：3
  • 2ELLINGTON C P. The novel aerodynamics of insect flight:applications to micro-air vehicles[J]. The Journal of Experimental Biology, 1999, 202: 3439-3448.
  • 3DICKINSON M H, LEHMANN F O, SANE S P. Wing rotation and the aerodynamic basis of insect flight[J]. Science,1999, 284: 1954-1960.
  • 4KUBO Y, SHIMOYAMA I, MIURA H. Study of insectbased flying microrobots[A]. IEEE International Conference on Robotics and Automation[C]. IEEE Computer Society Press, 1993, 2: 386-391.
  • 5SITTI M, CAMPOLO D, YAN J, et al. Development of PZT and PZN-PT bases unimorph actuators for micromechanical flapping mechanisms[A]. IEEE International Conference on Robotics and Automation[C]. IEEE Computer Society Press,2001:3839-3846.
  • 6SITFI M. PZT actuated four-bar mechanism with two flexible links for micromechanical flying insect thorax[A]. IEEE International Conference on Robotics and Automation[C].IEEE Computer Society Press, 2001: 3893-3900.

二级参考文献21

  • 1[1]Ellington C P. The novel aerodynamics of insect flight: applications to micro-air vehicles [J]. The Journal of Experimental Biology,1999, 202:3439-3448.
  • 2[2]Brich J M, Dickinson M H. Spanwise flow and the attachment of the leading-edge vortex on insect wings[J]. Nature, 2001,412:729 -733.
  • 3[4]Weis-Fogh T. Quick estimates of flight fitness in hovering animals, including novel mechanisms for lift production [J]. The Journal of Experimental Biology, 1973, 59: 169-230.
  • 4[5]Ellington C P, van den Berg C, Willmott A P. Leading edge vortices in insect flight[J]. Nature, 1996, 384:626 -630.
  • 5[6]Usherwood J R, Ellington C P. The aerodynamics of revolving wings Ⅰmodel hawkmoth wings[J]. The Journal of Experimental Biology, 2002, 205:1547 -1564.
  • 6[7]Usherwood J R, Ellington C P. The aerodynamics of revolving wings Ⅱpropeller force coefficients from mayfly to quail[J]. The Journal of Experimental Biology, 2002, 205: 1565 - 1576.
  • 7[8]Berg C V D, Ellington C P. The three-dimensional leading-edge vortex of a ‘hovering' model hawkmoth[J]. Philosophical Transactions of the Royal Society of London, 1997, 352:329 -340.
  • 8[9]Berg C V D, Ellington C P. The vortex wake of a ‘hovering' model hawmoth[J]. Philosophical Transactions of the Royal Society of London, 1997, 352:317-328.
  • 9[10]Dickinson M H, Gotz K G. Unsteady aerodynamic performance of model wing at low Reynolds numbers[J]. The Journal of Experimental Biology, 1993, 174:45 -64.
  • 10[11]Dickinson M H, Lehmann F-O, Sane S P. Wing rotation and the aerodynamic basis of insect flight[J]. Science, 1999, 284:1954 -1960.

共引文献2

同被引文献9

  • 1Grasmeyer M, Keennon T. Development of the black widow micro air vehicle[C]. Reno: American Institute of Aeronautics and Astronautics. Aerospace Sciences Meeting and Exhibit, 2001.
  • 2C P Ellington. The novel aerodynamics of insect flight: applica tions to microair vehieles[J]. Experimental Biology, 1999 (3) :3 439 - 3 448.
  • 3M H Dickinson, Lehmann F O, Sanjay P S. Wing rotation and the aerodynamic basis of insect flight [J ]. Science, 1999 (2) : 1 954-1 960.
  • 4Sun M, Tan J. Unsteady aerodynamic force generation by a model fruit fly wing[J]. Experimental Biology,2002(5):55- 70.
  • 5BRICH J M , DICKINSON M H. Spanwise flow and the attachment of the leading edge vortex on insect wings[ J ]. Nature,2001 (4):729 733.
  • 6Zaeem A. Khan. Design of flapping mechanisms based on trans-verse bending phenomena in insects [A], IEEE International Conference on Robotics and Automation[ C]. Washington DC . IEEE Press and IEEE Computer Society Press, 2006:2 323 - 2 328.
  • 7SITTIM. PZT actuated fourbar mechanism with two flexible links for micromechanical flying insect thorax[A]. IEEE International Conference on Robotics and Automation [ C]. Washington DC: IEEE Computer Society Press,2001:3 893 - 3 900.
  • 8Zaecm A Khan, S K Agrawal. Design of a mechanism for biaxial rotation of a wing for a hovering vehicle[J]. IEEE Transactions on mechatronics, 2006, 11 (2) : 145 - 153.
  • 9朱保利,昂海松,郭力.一种新型三维仿生扑翼机构设计与分析[J].南京航空航天大学学报,2007,39(4):457-460. 被引量：10

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制造业自动化
2005年 第2期

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