ACTA AERONAUTICAET ASTRONAUTICA SINICA >
Preliminary design method for miniature electric-powered vertical take-off and landing unmanned airial vehicle and effects of special parameters
Received date: 2016-11-24
Revised date: 2017-05-31
Online published: 2017-05-31
Supported by
National Natural Science Foundation of China (11402208)
The difficulties of the design of the miniature Electric-powered Vertical Take-Off and Landing Unmanned Aerial Vehicle (VTOL mEUAV) are analyzed,and a preliminary design method based on special parameters is proposed according to theoretical analysis.The choice of wing-load,estimation of total weight,the analysis of balance and control,and the design of tailless wing are described.The special parameters concerning power-to-weight ratio,propulsion matching and mounted incidence of a X-type tailless tail-sitter VTOL UAV equipped with one set of propulsion are then selected and analyzed.Based on the design results,the manufactory and flight tests are used to verify the design method.The results show that different design objective leads to different wing-load and power-to-weight ratio;propulsion efficiency and energy is greatly affected by motor and propeller matching;the suitable incidence of proplusion and deflected direction can improve the yaw control in hover without decreasing the whole property.
TANG Wei , SONG Bifeng , CAO Yu , YANG Wenqing . Preliminary design method for miniature electric-powered vertical take-off and landing unmanned airial vehicle and effects of special parameters[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017 , 38(10) : 220972 -220972 . DOI: 10.7527/S1000-6893.2017.220972
[1] 王冠林, 武哲. 垂直起降无人机总体方案分析及控制策略综合研究[J]. 飞机设计, 2006(3):25-30. WANG G L, WU Z. Configurations and control strategy for VTOL UAVs[J]. Aircraft Design, 2006(3):25-30(in Chinese).
[2] HOGEE J V. Development of a miniature VTOL tail-sitter unmanned aerial vehicle[D]. Provo:Brigham Young University, 2008:2-6.
[3] RAYMER D P. Aircraft design:A conceptual approach[M]. Reston, VA:AIAA Education, 1992:457-540.
[4] OOSEDO A, ABIKO S, KONNO A, et al. Development of a quad rotor tail-sitter VTOL UAV without control surfaces and experimental verification[C]//IEEE International Conference on Robotics and Automation ICRA. Piscataway, NJ:IEEE Press, 2013:317-322.
[5] OOSEDO A, KONNO A, MATSUMOTO T, et al. Design and attitude control of a quad-rotor tail-sitter vertical takeoff and landing unmanned aerial vehicle[J]. Advanced Robotics, 2012, 26(3-4):307-326.
[6] 张啸迟, 万志强, 章异赢, 等. 旋翼固定翼复合式垂直起降飞行器概念设计研究[J]. 航空学报, 2016, 37(1):179-192. ZHANG X C, WAN Z Q, ZHANG Y Y, et al. Conceptual design of rotary wing and fixed wing compound VTOL aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(1):179-192(in Chinese).
[7] 唐伟, 王进, 王利光, 等. 一种可变体X型机翼垂直起降微型飞行器:ZL201410233178.0[P]. 2014-08-13. TANG W, WANG J, WANG L G, et al. A VTOL MAV with morphing X-type wing:ZL201410233178.0[P]. 2014-08-13(in Chinese).
[8] KARAKAS H, KOYUNCU E, INALHAN G. ITU tailless UAV design[J]. Journal of Intelligent & Robotic Systems, 2013, 69(1-4):131-146.
[9] WAGNER N, BOLAND S, TAYLOR B, et al. Powertrain design for hand-launchable long endurance unmanned aerial vehicles[C]//47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Reston, VA:AIAA, 2011:5-6.
[10] HAROLD Y, MING C. Test, analysis and design of propeller propulsion systems for MAVs[C]//49th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Reston, VA:AIAA, 2011:2-18.
[11] 陈军, 杨树兴, 莫雳. 电动无人机动力系统建模与实验[J]. 航空动力学报, 2009, 24(6):1339-1344. CHEN J, YANG S X, MO L. Modeling and experimental analysis of UAV electric propulsion system[J]. Journal of Aerospace Power, 2009, 24(6):1339-1344(in Chinese).
[12] LANDOLFO G. Aerodynamic and structural design of a small nonplanar wing UAV[D]. Orlando, FL:University of Dayton, 2009:35-38.
[13] 王波, 侯中喜, 汪文凯. 小型电动垂直起降飞行器推进系统性能分析[J]. 国防科技大学学报, 2015(3):84-90. WANG B, HOU Z X, WANG W K. Performance analysis of propulsion system of miniature electric-powered vertical takeoff and landing air vehicles[J]. Journal of National University of Defense Technology, 2015(3):84-90(in Chinese).
[14] GUR O, ROSEN A. Optimizing electric propulsion systems for unmanned aerial vehicles[J]. Journal of Aircraft, 2009, 46(4):1340-1353.
[15] THOMAS J M, IFJU P G, KELLOGG J C, et al. Introduction to the design of fixed-wing micro air vehicles[M]. Reston, VA:AIAA, 2007:83-95.
[16] NICKEL K, WOHLFAHRT M. Tailless aircraft in theory and practice[M]. Reston, VA:AIAA, 1994:74.
[17] 段文博. 可悬停双旋翼微型飞行器设计与制造[D]. 南京:南京航空航天大学, 2008:10-16. DUAN W B. The design and manufactory of hovering dual rotor micro air vehicle[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 2008:10-16(in Chinese).
[18] RANDALL R, HOFFMANN C A, SHKARAYEV S. Longitudinal aerodynamics of a vertical takeoff and landing micro air vehicle[J]. Journal of Aircraft, 2015, 48(1):166-176.
[19] KHAN F A. Preliminary aerodynamic investigation of box-wing configurations using low fidelity codes[D]. Hamburg:Hamburg University, 2010:18-42.
[20] MELIN T. A vortex lattice MATLAB implementation for linear aerodynamic wing applications[D]. Stockholm:KTH Royal Institute of Technology, 2000:16-40.
[21] 刘斌, 马晓平, 王和平, 等. 小型电动无人机总体参数设计方法研究[J]. 西北工业大学学报, 2005, 23(3):396-400. LIU B, MA X P, WANG H P, et al. Design analysis methodology for electric powered mini UAV[J]. Journal of Northwestern Polytechnical University, 2005, 23(3):396-400(in Chinese).
/
| 〈 |
|
〉 |
CJA