自旋三旋翼飞行器的概念设计研究

doi:10.3969/j.issn.1009-086x.2020.04.04

现代防御技术 ›› 2020, Vol. 48 ›› Issue (4): 23-28.DOI: 10.3969/j.issn.1009-086x.2020.04.04

自旋三旋翼飞行器的概念设计研究

李泽波^a, 黄戈莹^b, 王轶轩^c, 方潮铭^c, 王奕霄^c, 李博雯^a

北京航空航天大学a.航空科学与工程学院; b.机械工程及自动化学院; c.仪器科学与光电工程学院,北京 100191

收稿日期:2019-10-15 修回日期:2020-02-26 出版日期:2020-08-20 发布日期:2021-01-21
作者简介:李泽波(1998-),男,广东揭阳人。硕士生,主要从事新型飞行器研究。通信地址:100191 北京市海淀区学院路37号北京航空航天大学 E-mail:boblee@buaa.edu.cn
基金资助:
全国大学生创新创业训练计划

Research on the Conceptual Design of Spinning Tricopter

LI Ze-bo^a, HUANG Ge-ying^b, WANG Yi-xuan^c, FANG Chao-ming^c, WANG Yi-xiao^c, LI Bo-wen^a

a.Beihang University,a.School of Aeronautic Science and Engineering; b.School of Mechanical Engineering and Automation; c.School of Instrumentation and Optoelectronic Engineering,Beijing 100191,China

Received:2019-10-15 Revised:2020-02-26 Online:2020-08-20 Published:2021-01-21

摘要/Abstract

摘要： 根据未来无人机发展的需求,提出了自旋的飞行方式,并设计了一款结构高度简化的自旋三旋翼飞行器。自旋三旋翼飞行器在飞行过程中,由于旋翼同向旋转产生的扭矩带动机身朝反方向自旋,在机翼处产生额外的升力,同时获得更好的稳定性。介绍了自旋三旋翼飞行器的概念设计,对自旋飞行的原理进行基本阐述,论证了其可行性,并基于此提出一种五自由度自旋飞行的控制方法,展望了其可能的应用场景。

关键词: 无人机, 飞行器设计, 飞行原理, 三旋翼, 自旋飞行器, 概念设计

Abstract: According to the future development of unmanned aerial vehicle (UAV),a new spinning flight mode is proposed,and a spinning tricopter with a highly simplified structure is designed.During the flight of the spinning tricopter,the torque generated by the rotation of the rotor in the same direction drives the fuselage to spin in the opposite direction,which generates additional lift at the wings while achieving better stability.The conceptual design of the spinning tricopter is introduced,the principle of spinning flight mode is analyzed,and its feasibility is demonstrated.Based on this new flight mode,a five-degree-of-freedom spin flight control method is proposed,and the outlook of its possible application is provided.

Key words: unmanned aerial vehicle (UAV), aircraft design, flying principle, tricopter, spinning aircraft, conceptual design

中图分类号:

V279

李泽波, 黄戈莹, 王轶轩, 方潮铭, 王奕霄, 李博雯. 自旋三旋翼飞行器的概念设计研究[J]. 现代防御技术, 2020, 48(4): 23-28.

LI Ze-bo, HUANG Ge-ying, WANG Yi-xuan, FANG Chao-ming, WANG Yi-xiao, LI Bo-wen. Research on the Conceptual Design of Spinning Tricopter[J]. Modern Defense Technology, 2020, 48(4): 23-28.

参考文献

[1] 付国强. 中程固定翼无人机发展综述及总体设计技术研究[C]//2019年(第四届)中国航空科学技术大会论文集,中国航空学会,2019:84-90.
FU Guo-qiang.Development Review of Mid-Range Fixed-Wing UAV and Study on Overall Design Technology[C]//2019(4th)China Aviation Science and Technology Conference,China Aviation Society,2019:84-90.
[2] 刘泽宇.无人直升机的价值和未来发展趋势[C]//2019年(第四届)中国航空科学技术大会论文集,中国航空学会,2019:410-420.
LIU Ze-yu.The Value and Future Development of Unmanned Helicopters[C]//2019 (4th) China Aviation Science and Technology Conference,China Aviation Society,2019:410-420.
[3] CHEN Fu-yang,JIANG Rong-qiang,ZHANG Kang-kang,et al.Robust Backstepping Sliding-Mode Control and Observer-Based Fault Estimation for a Quadrotor UAV[J].IEEE Transactions on Industrial Electronics,2016,63(8):5044-5056.
[4] XIAN Bin,HAO Wen.Nonlinear Robust Fault-Tolerant Control of the Tilt Trirotor UAV Under Rear Servo’s Stuck Fault:Theory and Experiments[J].IEEE Transactions on Industrial Informatics,2019,15(4):2158-2166.
[5] SALAZAR-CRUZ S,KENDOUL F,LOZANO R,et al.Real-Time Stabilization of a Small Three-Rotor Aircraft [J].IEEE Transactions on Aerospace and Electronic Systems,2008,44(2):783-794.
[6] Ali Zain Anwar,WANG Dao-bo,Aamir Muhammad.Fuzzy-Based Hybrid Control Algorithm for the Stabilization of a Tri-Rotor UAV[J].Academic Journal,2016,16(5):652-1-18.
[7] YOO D W,OH H D,WON D Y,et al.Dynamic Modeling and Stabilization Techniques for Tri-Rotor Unmanned Aerial Vehicles[J].International Journal of Aeronautical & Space Sciences,2010,11(3):167-174.
[8] Sergio Salazar-Cruz,Rogelio Lozano,Juan Escareño.Stabilization and Nonlinear Control for a Novel Trirotor Mini-Aircraft[J].Control Engineering Practice,2009,17(8):886-894.
[9] SERVAIS E,Brigitte d’Andréa-Novel,MOUNIER H.Ground Control of a Hybrid Tricopter[C]//2015 International Conference on Unmanned Aircraft Systems (ICUAS),2015:945-950.
[10] 《飞机设计手册》总编委会.飞机设计手册(第6册)[M].北京:航空工业出版社,2002.
Editorial Board of the Aircraft Design Manual.Aircraft Design Manual[M].Beijing:Aviation Industry Press,2002.
[11] John Seddon,Simon Newman.Basic Helicopter Aerodynamics[M].Wiley,2011:111-138.
[12] 郦正能.飞行器结构学[M].北京:北京航空航天大学出版社,2010:464.
LI Zheng-neng.Aircraft Structure[M].Beijing:Beihang University Press,2010:464.
[13] NIEMIEC R,GANDHI F.Multirotor Controls,Trim,and Autonomous Flight Dynamics of Plus- and Cross-Quadcopters[J].Journal of Aircraft,2017,54(5):1-11.
[14] 万佳,刘洪,王福新.多旋翼无人飞行器必要建模因素[J].北京航空航天大学学报报,2017,43(6):1072-1079.
WAN Jia,LIU Hong,WANG Fu-xin.Imperative Modeling Elements for Multi-Rotor Unmanned Aerial Vehicle [J].Journal of Beijing University of Aeronautics and Astronautics,2017,43(6):1072-1079.
[15] 方振平.航空飞行器飞行动力学[M].北京:北京航空航天大学出版社,2005:260-262.
FANG Zhen-ping.Flight Dynamics of Aerospace Vehicles[M].Beijing:Beihang University Press,2005:260-262.
[16] QUAN Quan.Introduction to Multicopter Design and Control[M].Springer Singapore,2017.
[17] 谢传锋,王琪.理论力学[M].北京:高等教育出版社,2015:453.
XIE Chuan-feng,WANG Qi.Theoretical Mechanics [M].Beijing:Higher Education Press,2015:453.
[18] 付强,李鸣,徐艳,等.试论民用无人机作为防空靶机的方法及可行性[J].教育教学论坛,2017(23):75-77.
FU Qiang,LI Ming,XU Yan,et al.Discussion on the Method and Feasibility of Civil UAV as Air Defense [J].Education and Teaching Forum,2017(23):75-77.
[19] 孙盛坤,禹琳琳.无人预警机系统发展思考[J].信息通信,2017(6):269-272.
SUN Sheng-kun,YU Lin-lin.The Development and Analysis for the Unnamed Airborne Warning and Control System [J].Information and Communications,2017(6):269-272.
[20] 刘媛媛.无人机遥感技术在生态环境领域中的应用[J].电子技术与软件工程,2016(20):119.
LIU Yuan-yuan.Application of UAV Remote Sensing Technology in Ecological Environment [J].Electronic Technology and Software Engineering,2016(20):119.
[21] 娄尚易,薛新宇,顾伟,等.农用植保无人机的研究现状及趋势[J].农机化研究,2017,39(12):1-6,31.
LOU Shang-yi,XUE Xin-yu,GU Wei,et al.Current Status and Trends of Agricultural Plant Protection Unmanned Aerial Vehicle [J].Research of Agricultural Mechanization,2017,39(12):1-6,31.
[22] 詹仁俊.电力巡检无人机通信中继系统的设计与实际应用[J].通讯世界,2017(3):210-211.
ZHAN Ren-jun.Design and Practical Application of Communication Relay System for Power Inspection UAV[J].Communications World,2017(3):210-211.
[23] 毛文军.无人机在气象服务中的应用[J].浙江气象,2016,37(4):38-40.
MAO Wen-jun.Application of UAV in Meteorological Services [J].Zhejiang Meteorology,2016,37(4):38-40.
[24] 杨中英,王毓龙,赖传龙.无人机蜂群作战发展现状及趋势研究[J].飞航导弹,2019(5):34-38.
YANG Zhong-ying,WANG Yu-long,LAI Chuan-long.Research on the Status Quo and Trend of UAV Bee Colony Operation[J].Aircraft Missiles,2019(5):34-38.
[25] 徐冠华.高空长航时无人机战场态势显示系统设计及效能评估研究[D].南昌:南昌航空大学,2016.
XU Guan-hua.Battlefield Situation Display System Design and Effectiveness Evaluation of HALE UAV[D].Nanchang:Nanchang University of Aeronautics,2016.
[26] 空天大鹏.无炸药武器缘何受特种作战青睐[N].中国航天报,2019-12-28(003).
Aerospace Dapeng:Why Non-Explosive Weapons Are Popular in Special Operations[N].China Aerospace News,2019-12-28(003).
[27] LI Heng,YE Zhang-yin .Effects of Rotational Motion on Dynamic Aeroelasticity of Flexible Spinning Missile with Large Slenderness Ratio[J].Aerospace Science and Technology,2019,94(1):1-14.
[28] 袁天保.弹道导弹滚动飞行动力学与控制研究[D].长沙:国防科学技术大学,2005.
YUAN Tian-bao.Research on Ballistic Missile Rolling Flight Dynamics and Control[D].Changsha:National University of Defense Technology,2005.

自旋三旋翼飞行器的概念设计研究

Research on the Conceptual Design of Spinning Tricopter

PDF (PC)

可视化

摘要/Abstract

引用本文

使用本文

参考文献

相关文章 15

编辑推荐

Metrics

本文评价

[1]	王瑞杰, 王得朝, 丰璐, 赵正党, 陈浙梁. 国外无人机蜂群作战样式进展及反蜂群策略研究[J]. 现代防御技术, 2023, 51(4): 1-9.
[2]	李碧燕, 胡顺. 基于方向信息的无人机群编队控制算法[J]. 现代防御技术, 2023, 51(2): 55-61.
[3]	王文涛, 甘旭升, 吴亚荣, 任谨慎, 王翠香. 考虑不确定性的低空无人机运行风险评估方法[J]. 现代防御技术, 2022, 50(5): 14-21.
[4]	宋占福, 赵全习, 胡文志, 黄懿. 无人机支援地面防空作战研究[J]. 现代防御技术, 2022, 50(5): 22-27.
[5]	周方宇, 周洁, 陈超波, 高嵩. 基于克隆免疫决策的无人机集群协同探测跟踪[J]. 现代防御技术, 2022, 50(5): 93-105.
[6]	董康生, 胡伟波, 沈雁鸣, 唐上钦. 美军无人空战装备智能化发展动态及启示[J]. 现代防御技术, 2022, 50(4): 28-37.
[7]	孙丰础, 甘旭升. 无人机双机空战对抗侧向机动路径规划[J]. 现代防御技术, 2022, 50(3): 109-118.
[8]	陈君一, 杨健. 通信对抗无人机集群侦察区域规划规则研究[J]. 现代防御技术, 2022, 50(1): 54-59.
[9]	刘玄冰, 周绍磊, 肖支才, 祁亚辉, 代飞扬. 固定翼无人机航迹跟踪抗风性研究[J]. 现代防御技术, 2022, 50(1): 41-47.
[10]	刘群, 杨昭, 周传霞. 某型旋翼无人机极限风速下运动失稳及失能特性研究[J]. 现代防御技术, 2022, 50(1): 19-24.
[11]	黄沛, 曹国辉, 张海晶, 张钧杰. 小型侦察无人机任务能力及拒止距离分析[J]. 现代防御技术, 2022, 50(1): 1-6.
[12]	马特, 郑致远, 赵军虎. 分布式多无人机编队控制与博弈算法研究[J]. 现代防御技术, 2021, 49(5): 45-50.
[13]	李勇, 李树豪, 党利. 基于鲁棒H_∞控制的无人机纵向自动驾驶仪设计[J]. 现代防御技术, 2021, 49(5): 32-44.
[14]	黄祥, 徐静, 都晨, 郭昭艺, 吴涛. 一种无人机辐射源调制样式识别算法[J]. 现代防御技术, 2021, 49(3): 98-104.
[15]	吴静, 蔡海锋, 刘俊良. 纳卡地区冲突无人机攻防运用分析及地空反无人对策建议[J]. 现代防御技术, 2021, 49(3): 13-20.