Characteristics of Quadrotor UAV in Forward Flying Mode
YE Jianchuan1, WANG Jiang1, LIANG Yi2, SONG Tao1, WU Zeliang1, XU Chao1,3
(1.School of Aerospace Engineering,Beijing Institute of Technology,Beijing 100081,China;2.Equipment Development Department,Beijing 100035,China;3.Beijing Special Mechanical and Electrical Research Institute,Beijing 100089,China)
YE Jianchuan, WANG Jiang, LIANG Yi, SONG Tao, WU Zeliang, XU Chao. Characteristics of Quadrotor UAV in Forward Flying Mode[J]. Acta Armamentarii, 2021, 42(11): 2476-2490.
[1] AMEZQUITA-BROOKS L,LICEAGA-CASTRO E,GONZALEZ-SANCHEZ M,et al.Towards a standard design model for quadrotors: a review of current models,their accuracy and a novel simplified model[J].Progress in Aerospace Sciences,2017,95:1- 23. [2] SAEED A,YOUNES A B,CAI C,et al.A survey of hybrid unmanned aerial vehicles[J].Progress in Aerospace Sciences,2018,98:91-105. [3] PINES D J,BOHORQUEZ F.Challenges facing future micro-air-vehicle development[J].Journal of Aircraft,2006,43(2):290-305. [4] BRISTEAU P J,MARTIN P,SALAN E,et al.The role of propeller aerodynamics in the model of a quadrotor UAV[C]∥Proceedings of the 2009 European Control Conference. Budapest,Hungary:IEEE,2009:683-688, [5] JIANG T,LIN D F,SONG T.Finite-time backstepping control for quadrotors with disturbances and input constraints[J].IEEE Access,2018,6:62037-62049. [6] AMEZQUITA-BROOKS L,HERNANDEZ-ALCANTARA D,SANTANA-DELGADO C,et al.Improved model for micro-UAV propulsion systems:characterization and applications[J].IEEE Transactions on Aerospace and Electronic Systems,2020,56(3):2174-2197. [7] HOFFMANN G M,HUANG H M,WASLANDER S L,et al.Quadrotor helicopter flight dynamics and control:theory and experiment[C]∥Proceedings of the AIAA Guidance,Navigation and Control Conference and Exhibit. Hilton Head,SC,US:AIAA,2007:6461. [8] 吕品,赖际舟,杨天雨,等.基于气动模型辅助的四旋翼飞行器室内自主导航方法[J].航空学报,2015,36(4):1275-1284. L P,LAI J Z,YANG T Y,et al.Autonomous navigation method aided by aerodynamics model for an indoor quadrotor[J].Acta Aeronautica et Astronautica Sinica,2015,36(4):1275-1284. (in Chinese) [9] 夏青元,徐锦法.三轴式无人旋翼飞行器及自适应飞行控制系统设计[J].航空学报,2013,34(3): 495-508. XIA Q Y,XU J F.A design of triaxial unmanned rotor aircraft and its adaptive flight control system[J].Acta Aeronautica et Astronautica Sinica,2013,34(3): 495-508. (in Chinese) [10] YE J C,WANG J,HE S M,et al.Rotor performance analysis and modeling of multirotor using wind-tunnel test[C]∥Proceedings of the 2020 International Conference on Unmanned Aircraft Systems.Athens,Greece: IEEE, 2020:1644-1649. [11] THEYS B,DIMITRIADIS G,HENDRICK P,et al.Experimental and numerical study of micro-aerial-vehicle propeller performance in oblique flow[J].Journal of Aircraft,2017,54(3):1076-1084. [12] KOLAEI A,BARCELOS D,BRAMESFELD G.Experimental analysis of a small-scale rotor at various inflow angles[J/OL].International Journal of Aerospace Engineering,2018[2020-11-25]. https:∥doi.org/10.1155/2018/2560370. [13] HWANG J Y,JUNG M K,KWON O J.Numerical study of aerodynamic performance of a multirotor unmanned-aerial-vehicle configuration[J].Journal of Aircraft,2015,52(3): 839-846. [14] ORSAG M,BOG S. Influence of forward and descent flight on quadrotor dynamics[J/OL].Recent Advances in Aircraft Technology,2012:141-156[2020-11-25].https:∥www.intechopen.com/books/recent-advances-in-aircraft-technology/influence-of-forward-and-descent-flight-on-quadrotor-dynamics. [15] TURPIN M,MICHAEL N,KUMAR V.Trajectory design and control for aggressive formation flight with quadrotors[J].Autonomous Robots,2012,33:143-156. [16] BARCELOS D,KOLAEI A,BRAMESFELD G.Aerodynamic interactions of quadrotor configurations[J].Journal of Aircraft,2020,57(1):1-17. [17] MISIOROWSKI M,GANDHI F,OBERAI A A.Computational study on rotor interactional effects for a quadcopter in edgewise flight[J].AIAA Journal,2019,57(12):5309-5319. [18] LUO J L,ZHU L F,YAN G R.Novel quadrotor forward-flight model based on wake interference[J].AIAA Journal,2015,53(12): 3522-3533. [19] KAYA D,KUTAY A T.Aerodynamic modeling and parameter estimation of a quadrotor helicopter[C]∥Proceedings of the AIAA Atmospheric Flight Mechanics Conference.Atlanta,GA,US:AIAA,2014: 2558. [20] REMPLE R K,TISCHLER M B.Aircraft and rotorcraft system identification[M].2nd ed. Blacksburg,VA,US:A IAA,2006:433-450. [21] DROANDI G,GIBERTINI G,GRASSI D,et at.Proprotor-wing aerodynamic interaction in the first stages of conversion from helicopter to aeroplane mode[J]. Aerospace Science and Technology,2016,58:116-133. [22] PADFIELD G D. Helicopter flight dynamics including a treatment of tiltrotor aircraft[M].3rd ed. Hoboken,NJ,US:John Wiley & Sons Inc.,2018. [23] 宋保维,张姜军,杜晓旭,等.四旋翼碟形自主水下航行器运动方程建立与流体特性仿真研究[J].兵工学报,2016,37(2): 299-306. SONG B W,ZHANG J J,DU X X,et at.Estimation of equation of motion of four-rotor dish-shaped AUV and simulation research on its hydrodynamic characteristics[J].Acta Armamentarii,2016,37(2): 299-306. (in Chinese) [24] THEYS B,DIMITRIADIS G,ANDRIANNE T,et al. Wind tunnel testing of a VTOL MAV propeller in tilted operating mode[C]∥Proceedings of the 2014 International Conference on Unmanned Aircraft Systems. Orlando,FL,US:IEEE,2014: 1064-1072. [25] 薛晓明,杨长江.无刷直流电机建模研究[J].电机与控制学报,2009,13(6):874-885. XUE X M,YANG C J.Study of modeling for brushless DC motor drives[J].Journal of Motor and Control,2009,13(6):874-885.(in Chinese)