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弹箭与制导学报 >

2021 , Vol. 41 >Issue 6: 23 - 28

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2021.06.005

基于增益调度法的倾转旋翼控制系统设计

  • 宋晓东 ,
  • 吴斌 ,
  • 桑涛
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  • 北京理工大学宇航学院,北京 100081

宋晓东(1979—),男,北京人,副教授,博士,研究方向:空间机器人及微重力模拟方法与技术、伺服控制技术及应用。

收稿日期: 2019-11-18

  网络出版日期: 2025-02-07

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Design of Tilting Rotor Control System Based on Gain Scheduling Method

  • SONG Xiaodong ,
  • WU Bin ,
  • SANG Tao
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  • School of Aerospace Engineering,Beijing Institute of Technology,Beijing 100081,China

Received date: 2019-11-18

  Online published: 2025-02-07

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摘要

针对无人机倾转四旋翼无人机的动力学模型进行分析,以倾转角度为调度参量设计了增益调度控制器,并通过MATLAB软件在平衡点处进行极点配置,计算获得各个平衡点的控制参数。引入速度自适应项,以解决线性化模型时存在的误差;采用误差四元数方法作为控制器的输入量,避免了垂直起降过程中欧拉角奇异问题;通过实验表明该方法具有较好的控制效果。

关键词： 无人机; 飞行控制; 增益调度; 四元数

本文引用格式

宋晓东 , 吴斌 , 桑涛 . 基于增益调度法的倾转旋翼控制系统设计[J]. 弹箭与制导学报, 2021 , 41(6) : 23 -28 . DOI: 10.15892/j.cnki.djzdxb.2021.06.005

Abstract

Analyzing the dynamic model of the tilting four rotor, the gain scheduling controller is designed with tilting angle as the scheduling parameter, with pole allocation by MATLAB software at the equilibrium point, calculating to obtain the control parameters of each equilibrium point. Speed adaptive term is introduced to solve the error in linearization model. The error quaternion method is used as the input of the controller to avoid the ruler angle singular problem while the vertical take-off and landing. Experiments show that this method has better control effect.

Key words： UAV; flight control; gain scheduling; quaternion

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参考文献

原文顺序 | 文献年度倒序 | 文中引用次数倒序
[1]
路平, 肖文健. 倾转机身无人机俯仰角奇异问题研究[J]. 飞行力学, 2013, 31(5):429-432.

[2]
潘震, 池程芝, 张竞凯, 等. 基于自抗扰滑模理论的倾转旋翼飞行器非线性姿态控制研究[J]. 航空兵器, 2018(6):44-49.

[3]
张飞, 路平, 江涛, 等. 基于模糊控制的倾转三旋翼无人机过渡模式操纵策略研究[J]. 电光与控制, 2018, 25(4):32-36.

[4]
FRANCESCO G D, MATTEI M, EGIDIO D. Incremental nonlinear dynamic inversion and control allocation for a tilt rotor UAV[C]// AIAA. Proceedings of AIAA Guidance, Navigation, and Control Conference. Reston: AIAA, 2014: 13-17.

[5]
陈晓, 王晓燕, 王新民, 等. 改进的倾转旋翼机平稳过渡控制系统设计[J]. 计算机工程与应用, 2019, 155(21):253-259.

[6]
唐胜景, 李梦婷, 刘真畅, 等. 串置翼垂直起降无人机过渡机动飞行控制[J]. 系统工程与电子技术, 2019, 41(6):1342-1350.

DOI

[7]
HUSAIN Z, ABDULLAH M Z, YAP T C. Two-dimensional analysis of tandemstaggered airfoils using computational fluid dynamics[J]. International Journal of Mechanical Engineering Education, 2005, 33(3): 195-207.

[8]
鲁可, 刘春生, 汪正中, 等. 倾转旋翼飞行器飞行力学建模及验证分析[J]. 系统工程与电子术, 2017, 39(4):910-916.

[9]
范和平. 基于QFT的倾转旋翼飞行器控制律设计[D]. 南京: 南京航空航天大学, 2017.

[10]
高阳, 吴文海, 周思羽. 垂直/短距起降飞机非线性动力学建模与仿真[J]. 哈尔滨工业大学学报, 2019, 51(4):115-122.

[11]
蒋睿, 魏蛟龙, 岑朝辉. 基于四元数反馈的卫星姿态控制系统仿真模型建立[J]. 系统仿真学报, 2009, 21(19):6260-6265.

[12]
AHMED J, VINCENT T C, BERNSTEIN D S. Adaptive asymptotic tracking of spacecraft attitude motion with inertia matrix identification[J]. Journal of Guidance, Control and Dynamics, 1998, 21(5): 684-691.

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