Duan Jingyuan, Zhang Chunxi, Shi Jieqinet al. QoS analysis on IEEE- 1394b fiber optical bus system[J]. Journal of Beijing University of Aeronautics and Astronautics, 2008, 34(04): 396-399. (in Chinese)
Citation: Gong Maozhen, Yuan Peijiang, Wang Tianmiao, et al. Intelligent verticality-adjustment method of end-effector in aeronautical drilling robot[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(10): 1400-1404. (in Chinese)

Intelligent verticality-adjustment method of end-effector in aeronautical drilling robot

  • Received Date: 12 Oct 2011
  • Publish Date: 30 Oct 2012
  • Based on the requirement of robotic drilling for aircraft fuselage, a novel verticality adjustment method of drill bit in aeronautical drilling robot system was proposed, which is composed of surface-normal measurement and adjustment of drill bit-s attitude. Three laser range sensors were used in surface-normal measurement to measure the distances between sensors and three measurement positions around the drilling point. Thus the normal vector can be calculated from the cross product of any two vectors that are tangent to the surface at the drilling point. Meanwhile, the angle between normal vector and drill bit was obtained, which was fed back to the control system. Finally, the attitude of drill bit was adjusted using the binary angular adjustment mechanism (BAAM) to correct drill bit in line with the normal vector, which ensures to drill along the normal direction of drilling point. The high-accuracy, high-efficiency and practicability of the verticality adjustment method were tested by the experiments conducted on the aeronautical drilling robot, which meet the requirements of the auto-drilling for aircraft manufacturing.

     

  • [1]
    Bakuckas J G,Bigelow C A,Tan P W.Characterization of fatigue behaviour of aircraft fuselage structure //Proceedings of the 22nd Symposium of the International Committee on Aeronautical Fatigue.Lucern,Switzerland:EMAS,2003:5-9
    [2]
    Wang Min,Xue Shaoding,Jiang Hongyu,et al.Development of knowledge-based system on aircraft assembly drilling process //IEEE International Conference on Information Science and Engineering(ICISE).Hangzhou:IEEE,2010:1-4
    [3]
    Proppe C.Probabilistic analysis of multi-site damage in aircraft fuselages[J].Computational Mechanics,2003,30(4):323-329
    [4]
    Lutters W G,Ackerman M S.Achieving safety:a field study of boundary objects in aircraft technical support //Proceedings of ACM conference on Computer Supported Cooperative Work.New York:ACM,2002:266-275
    [5]
    Devlieg R,Szallay T.Applied accurate robotic drilling for aircraft fuselage[J].SAE International Journal of Aerospace,2010,3(1):180-186
    [6]
    Hasegawa N,Okada T,Shimizu T.Measurement of surface-normal using a range sensor with a pair of wedge-prisms //IEEE International Conference on Instrumentation and Measurement Technology (IMTC).Ottawa,Canada:IEEE,2005,1744-1749
    [7]
    应高明,王仲奇,康永刚,等.飞机壁板自动钻铆法向量测量方法研究[J].机床与液压,2010,38(20):1-4 Ying Gaoming,Wang Zhongqi,Kang Yonggang,et al.Study on normal vector measurement method in auto-drilling and riveting of aircraft panel[J].Machine Tool & Hydraulics,2010,38(20):1-4(in Chinese)
    [8]
    蔺小军,王增强,单晨伟.自由曲面CMM测量测头半径补偿方法[J].航空制造技术,2011(10):75-77,85 Lin Xiaojun,Wang Zengqiang,Shan Chenwei.Method of probe radius compensation for free surface measurement[J].Aeronautical Manufacturing Technology,2011(10):75-77,85(in Chinese)
    [9]
    Page D L,Sun Y,Koschan A F,et al..Normal vector voting:crease detection and curvature estimation on large,noisy meshes[J].Graphical Models,2002,64:199-229
    [10]
    秦现生,汪文旦,楼阿莉,等.大型壁板数控钻铆的三点快速调平算法[J].航空学报,2007,28(6):1455-1460 Qin Xiansheng,Wang Wendan,Lou Ali,et al.Three-point bracket regulation algorithm for drilling and riveting of aerofoil[J].Acta Aeronautica et Astronautica Sinica,2007,28(6):1455-1460(in Chinese)
    [11]
    夏长洪.一种带角度自动调节装置的钻孔设备:中国,201833210U .2011-5-18 Xia Changhong.A drilling equipment with automatic angle adjustment:China,201833210U .2011-5-18(in Chinese)
    [12]
    Gerald F.Curves and surface for CAGD:a practical guide[M].San Francisco:Morgan Kaufmann,2002:261-263
    [13]
    Jin Shuangshuang,Lewis R,West D.A comparison of algorithms for vertex normal computation[J].The Visual Computer,2005,21(1/2):71-82
    [14]
    Klasing K,Althoff D,Wollherr D,et al.Comparison of surface normal estimation methods for range sensing applications //IEEE International Conference on Robotics and Automation (ICRA).Kobe:IEEE,2009:3206-3211
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