多旋翼飞行器的可控度分析

doi:10.7527/S1000-6893.2017.721561

Abstract

Abstract:

The degree of controllability of multi-rotors was solved to evaluate the control levels of the aircraft system,based on the approximation calculation method of controllability proposed by George Klein et al. Firstly, variations of the degree of controllability were analyzed under three conditions of one steering gear broken down, one motor breakoff and the normal flight respectively on the variable-pitch quadrotor.And then with the comparative analysis of variable-pitch and fixed-pitch of four, six and eight rotors, the results showed that the degree of controllability of the system was positively correlated with the number of the rotors. Finally, the conception of degree of controllability was applied to two kinds of hybrid-electric hexacopter compared with the conventional electric hexacopter with fixed-pitch. And the research results indicated that the proper configuration could improve the degree of controllability remarkably.

Key words: degree of controllability, variable-pitch multi-rotor, fixed-pitch, failure mode, hybrid-electric

CLC Number:

V219

ZHAO Qibing, LIU Yong. Analysis of degree of controllability with multi-rotor aircraft[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(S1): 721561-721561.

References

[1] KALMAN R. On the general theory of control systems[J]. IRE Transactions on Automatic Control, 1959, 4(3): 110.
[2] VISWANATHAN C N, LONGMAN R W, LIKINS P W. A degree of controllability definition-fundamental concepts and application to modal systems[J]. Journal of Guidance, Control, and Dynamics, 1984, 7(2): 222-230.
[3] 杜光勋, 全权. 输入受限系统的可控度及其在飞行控制中的应用[J]. 系统科学与数学, 2014, 34(12): 1578-1594. DU G X, QUAN Q. Degree of controllability and its application in aircraft flight control[J]. Journal of System Science and Mathematical Science, 2014, 34(12): 1578-1594 (in Chinese).
[4] YANG B, DU G, QUAN Q, et al. The degree of controllability with limited input and an application for hexacopter design[C]//2013 32nd Chinese Control Conference. Xi'an: Northwestern Polytechnical University, 2013: 113-118.
[5] KLEIN G, ONGAMAN R W, INDBERG R E. Computation of a degree of controllability via system discretization[J]. Journal of Guidance, Control, and Dynamics, 1982, 5(6): 583-588.
[6] 岳基隆, 张庆杰, 朱华勇. 微小型四旋翼无人机研究进展及关键技术浅析[J]. 电光与控制, 2010, 17(10): 46-52. YUE J L, ZHANG Q J, ZHU H Y. Research progress and key technologies of micro quadrotor UAVs[J]. Electronics Optics and Control, 2010, 17(10): 46-52 (in Chinese).
[7] SCARAMUZZA D. Aggressive quadrotor flight through narrow gaps with onboard sensing and computing using active vision[C]//Proceeding of the IEEE International Conference on Robotics and Automation (ICRA). Piscataway, NJ: IEEE Press, 2017.
[8] 宿敬亚, 樊鹏辉, 蔡开元. 四旋翼飞行器的非线性 PID 姿态控制[J]. 北京航空航天大学学报, 2011, 37(9): 1054-1058. SU J Y, FAN P H, CAI K Y. Attitude control of quadrotor aircraft cia nonlinear PID[J]. Journal of Beijing University of Aeronautics and Astromautics, 2011, 37(9): 1054-1058 (in Chinese).
[9] 范云生, 曹亚博, 赵永生. 四旋翼飞行器轨迹跟踪控制器的设计与验证[J]. 仪器仪表学报, 2017, 38(3): 741-749. FAN Y S, CAO Y B, ZHAO Y S. Design and validation of trajectory tracking controller for quadrotor[J]. Chinese Journal of Scientific Instrument, 2017, 38(3): 741-749 (in Chinese).
[10] ISWANTO I, WAHYUNGGORO O, CAHYADI A I. Quadrotor path planning based on modified fuzzy cell decomposition algorithm[J]. Telecommunication Computing Electronics and Control, 2016, 14(2): 655-664.
[11] 吕亮. 具有执行器饱和的控制系统分析与设计[D]. 上海: 上海交通大学, 2010: 2-9. LU L. Analysis and design of control systems in the presence of actuator saturation[D].Shanghai: Shanghai Jiao Tong University, 2010: 2-9 (in Chinese).
[12] CIESLAK J, HENRY D, ZOLGHADRI A. Fault tolerant flight control: From theory to piloted flight simulator experiments[J]. IET Control Theory & Applications, 2010, 4(8): 1451-1464.
[13] VALENTI M, BETHKE B, FIORE G, et al. Indoor multi-vehicle flight testbed for fault detection,isolation, and recovery[C]//AIAA Guidance, Navigation, and Control Conference and Exhibit. Reston, VA: AIAA, 2006.
[14] GORDON L J. Principles of helicopter aerodynamics[M]. Cambridge: Combridge University Press, 2000: 115-124.
[15] BOUABDALLAH S. Design and control of quadrotors with application to autonomous flying[D]. Lausanne: Swiss Federal Institute of Technology in Lausanne, 2007: 16-18.
[16] POUNDS P, MAHONY R, CORKE P. Modelling and control of a large quadrotor robot[J]. Control Engineering Practice, 2010, 18(7): 691-699.
[17] CUTLER M J. Design and control of an auton-omous variable-pitch quadrotor helicopter[D]. Massachusetts: Massachusetts Institute of Technology, 2012: 34-41.
[18] CUTLER M, URE N K, MICHINI B, et al. Comparison of fixed and variable pitch actuators for agile quadrotors[C]//AIAA Guidance, Navigation, and Control Conference. Reston, VA: AIAA, 2011.
[19] BRESCIANI T. Modelling, identification and control of a quadrotor helicopter[D]. Lund: Lund University, 2008: 22-27.
[20] HEMATI N, LEU M C. A complete model characterization of brushless DC motors[J]. IEEE Transactions on Industry Applications, 1992, 28(1): 172-180.

Analysis of degree of controllability with multi-rotor aircraft

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[14]	Feng Yuansheng;Dong Cong. A METHOD FOR IDENTIFYING SIGNIFICANT FAILURE MODES OF A STRUCTURAL SYSTEM [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1991, 12(9): 537-541.
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