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基于改进PSO的无人自转旋翼机二自由度PID飞行控制 被引量:7

Flight Control of Two-degree-of-freedom PID Unmanned Gyrocopter Based on Improved PSO
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摘要 针对传统无人自转旋翼机自动控制采用一自由度PID和优化算法相结合,因自转旋翼机的响应滞后特性,一自由度PID不能同时满足快速响应和抑制干扰的问题,提出基于粒子群算法和模拟退火算法的二自由度PID控制器,同时设计前馈控制器的降噪方法,实现对无人自转旋翼机的有效控制。通过搭建Matlab仿真模型验证其可行性,其仿真结果表明本研究中算法相对于传统一自由度PID控制响应速度较快,前馈控制器能有效地抑制外部干扰,鲁棒性强,且系统响应速度快,响应时间提升约11%,响应精度更高,收敛误差小,约是传统PID的1/6,控制系统更稳定。同时在2种不同飞行环境下实际飞行实验验证了基于PSO-SA的二自由度PID控制器可行性,可为无人自转旋翼机在农业航空领域中的应用提供理论基础。 For the automatic control of the traditional unmanned autogyro,a combination of one-degree-of-freedom PID and optimization algorithm is used,because the one-degree-of-freedom PID cannot solve the problem of fast response and interference suppression at the same time due to the response lag characteristics of autogyro.A two-degree-of-freedom PID controller based on the particle swarm algorithm and the simulated annealing algorithm is proposed,and a noise reduction method of feedforward controller is designed to achieve effective control of unmanned autogyro.The feasibility is verified by building a Matlab simulation model.The simulation results show that the response speed of the algorithm in this study is faster than that of the traditional one-degree-of-freedom PID control.The feedforward controller,with strong robustness and system response can effectively suppress external disturbances.As the result,the speed is fast and the response time is increased by about 11%.The control system is more stable with higher response accuracy and slighter convergence error value.The possibility of error is about 1/6 lower than the traditional PID.At the same time,the actual flight experiments in two different flight environments verified the feasibility of the two-degree-of-freedom PID controller based on PSO-SA,which can provide a theoretical basis for the application of unmanned autogyro in the field of agricultural aviation.
作者 苏中滨 张磊磊 马铮 高睿 SU Zhongbin;ZHANG Leilei;MA Zheng;GAO Rui(School of Electrical and Information,Northeast Agricultural University,Harbin 150030,China)
出处 《农业机械学报》 EI CAS CSCD 北大核心 2022年第1期151-158,185,共9页 Transactions of the Chinese Society for Agricultural Machinery
基金 黑龙江省“百千万”工程科技重大专项(2019ZX14A04) 国家重点研发计划项目(2016YFD0300610)。
关键词 自转旋翼机 自动控制 二自由度 PID 粒子群算法 模拟退火算法 gyrocopter automatic control two-degrees-of-freedom PID particle swarm algorithm simulated annealing algorithm
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  • 1朱清华,李建波,倪先平,张呈林.旋翼机总体设计的几个问题[J].航空科学技术,2006(5):28-32. 被引量:13
  • 2王适存 航空专业教材编审组.直升机空气动力学[M].,1985.. 被引量:9
  • 3薛定宇.控制系统仿真与计算机辅助设计[M].北京:机械工业出版社,2006:124-128. 被引量:4
  • 4Leishman J G. Development of the autogyro: a technical perspective[J]. Journal of Aircraft, 2004, 41 (4): 765-781. 被引量:1
  • 5Vladislav Gavrilets. Autonomous Aerobatic Maneuvering of Miniature Helicopters[D]. Massachusetts Institute of Technology, 2003. 被引量:1
  • 6Srikanth S-, Gaurav S, Sukhatme, et al. An Experimental Study of the Autonomous Helicopter Landing Problem[J]. Springer Tracts in Advanced Robotics, 2003(5): 466-475. 被引量:1
  • 7Setlur P, Dawson D, Fang Y, et al. Nonlinear tracking control of the VTOL aircraft[C]. Proc of the 40th IEEE Conf.on Decision and Control.Orlando: IEEE Society, 2001: 4592-4597. 被引量:1
  • 8Spanoudakis P, Tsourveloudis N C, Valavanis K P. Design specifications for an unmanned VTOL[C]. Proc. of the 2004 IEEE Int. Conf.on Robotics and Automation. New Orleans: IEEE Society, 2004: 3616-3621. 被引量:1
  • 9Hollmann M. Modem Gyroplane Design[M]. Minterey, 1992. 被引量:1
  • 10Leishman J G. Development of the Autogyro a Technical Perspective[J]. Journal of Aircraft, 2004, 41(4): 765-781. 被引量:1

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