Kewei Li,∗ Bianhong Li,∗∗ Dongfang Li,∗∗ Chao Wang,∗∗∗ and Hongbin Deng∗∗


  1. [1] J.R. Reinhardt, J.E. James, and E.M. Flanagan, Future em-ployment of UAVs: Issues of jointness, Essay Contest onMilitary Innovation, 1, 1999, 36–41.
  2. [2] Z. Shahid and A. Rashid, Applications of UAV in daily life,54th AIAA Aerospace Sciences Meeting, San Diego, CA, 2016.
  3. [3] D. Jiatao, X. Xiaohui, and W. Yang, An adaptive feedfor-ward control method for under-actuated bipedal walking onthe compliant ground, International Journal of Robotics andAutomation, 32(1), 2017, 63–77.
  4. [4] G. Garcea, A. Madeo, and G. Zagari, Asymptotic post-bucklingFEM analysis using corotational formulation, InternationalJournal of Solids & Structures, 46(2), 2009, 377–397.
  5. [5] H. Gao, Y. Zhang, Q. Wu, and J. Song, An analytical modelfor predicting the machining deformation of a plate blankconsiders biaxial initial residual stresses, The InternationalJournal of Advanced Manufacturing Technology, 93(1–4), 2017,1473–1486.
  6. [6] H.-J. Gao, Y.-D. Zhang, Q. Wu, and J. Song, Experimentalinvestigation on the fatigue life of Ti–6Al–4V treated byvibratory stress relief, Metals (Basel), 7(5), 2017, 158:1–13.
  7. [7] K. Choi, M.S. Chun, C.J.V. Tyne, et al., Optimization of opendie forging of round shapes using FEM analysis, Journal ofMaterials Processing Technology, 172(1), 2006, 88–95.
  8. [8] B.H. Xia, Z.S. Chen, T.L. Li, Y.D. Yang, Y. Li, and L. Mei,Construction control of a long span cable-stayed rail transitbridge, International Journal of Robotics and Automation, 32,2017, 274–282.
  9. [9] H. Hongli, W. Dingwen, G. Puyun, and G. Jian, Finite elementanalysis of composites wings of UAV, Proc. 20th NationalConference on Structural Engineering, Ning Bo, Zhe Jiang, 1,2011 195–198.
  10. [10] X. Sun and J. Zhang, Effect of the reinforced leading or trailingedge on the aerodynamic performance of a perimeter-reinforcedmembrane wing, Journal of Fluids and Structures, 68, 2017,90–112.
  11. [11] J. Nianchao, Z. Guangmin, Z. Xiong, D. Yong, and Z. Zhiqing,The three-dimensional finite element analysis and the exper-imental study about the main spar of UAV wings, ModernManufacturing Engineering, (6), 2011, 1–4.
  12. [12] N.I. Ismail, A.H. Zulkifli, M.Z. Abdullah, M. Hisyam Basri,and N. Shah Abdullah, Computational aerodynamic analysison perimeter reinforced (PR)-compliant wing, Chinese Journalof Aeronautics, 26(5), 2013, 1093–1105.
  13. [13] C. Wei-wei and C. Wan-ji, On the simulation of UAV compositestructure and it’s analysis by FEM, Aircraft Design, 32(1),2012, 15–18.
  14. [14] W. Wei, Z. Zhou, Z. Xiaoping, and W. Rui, Static aeroe-lastic characteristics analysis of a very flexible solar pow-ered UAV with geometrical nonlinear effect considered, Jour-nal of Northwestern Polytechnical University, 32(4), 2014,499–504.
  15. [15] Y. Xingyan, F. Zhenyu, and L. Xiang, Finite element analysisof composite wing for unmanned aerial vehicle based on MSC.Nastran, Fiber Reinforced Plastics/Composites, 31(1), 2010,3–6.
  16. [16] W. Zhiwen, W. Bin, Z. Xing, Z. Ping, and C. Lin, Mechanicalsimulation analysis of a quad-rotor unmanned aerial vehicle,Electro-Mechanical Engineering, 32(1), 2016, 52–54.
  17. [17] A. Mancini, A. Cesetti, A. Iuale, E. Frontoni, P. Zingaretti,and S. Longhi, A framework for simulation and testing of UAVsin cooperative scenarios, Journal of Intelligent and RoboticSystems, 54(1–3), 2009, 307–329.
  18. [18] M.D. Maughmer, T.S. Swan, and S.M. Willits, Design andtesting of a winglet airfoil for low-speed aircraft, Journal ofAircraft, 39(4), 2002, 654–661.
  19. [19] L.F. Gonzalez, J. Periaux, L. Damp, and K. Srinivas, Evolu-tionary methods for multidisciplinary optimization applied tothe design of UAV systems, Engineering Optimization, 39(7),2007, 773–795.
  20. [20] P. Sandoval, P. Cornejo, and F. Tinapp, Evaluating thelongitudinal stability of an UAV using a CFD-6DOF model,Aerospace Science and Technology, 43, 2015, 463–470.
  21. [21] P. Panagiotou, P. Kaparos, and K. Yakinthos, Winglet designand optimization for a MALE UAV using CFD, AerospaceScience and Technology, 39, 2014, 190–205.
  22. [22] J. Verbeke and S. Debruyne, Vibration analysis of a UAV mul-tirotor frame, International Conference on Noise and VibrationEngineering, Leuven, Belgium, 2016.
  23. [23] T. Scott, H. David, T. Giuseppe, and G. Santiago, CFDsimulation of a quad-rotor UAV with rotors in motion explicitlymodeled using an LBM approach with adaptive, AIAA Scienceand Technology Forum and Exposition, Grapevine, TX, 2017.
  24. [24] Y. Shenghui, L. Xingxing, C. Bingtai, L. Shixiong, and Z.Yongjun, CFD models and verification of the downwash airflowof an eight-rotor UAV, ASABE 2019 Annual InternationalMeeting, Boston, MA, 2019.
  25. [25] Z.S. Chen, J.T. Zhou, G. Hu, Y. Li, H. Ma, and G.W. Yao,A novel movable scaffolding system (MSS) for a long-spancurved girder bridge, International Journal of Robotics andAutomation, 32(2), 2017, 164–175.

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