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基于LADRC的直升机姿态解耦控制及参数整定

吴超 王浩文 姜辰 张玉文 倪先平

吴超, 王浩文, 姜辰, 等 . 基于LADRC的直升机姿态解耦控制及参数整定[J]. 北京航空航天大学学报, 2015, 41(11): 2085-2094. doi: 10.13700/j.bh.1001-5965.2014.0710
引用本文: 吴超, 王浩文, 姜辰, 等 . 基于LADRC的直升机姿态解耦控制及参数整定[J]. 北京航空航天大学学报, 2015, 41(11): 2085-2094. doi: 10.13700/j.bh.1001-5965.2014.0710
WU Chao, WANG Haowen, JIANG Chen, et al. LADRC-based attitude decoupling control for helicopter and parameters tuning[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(11): 2085-2094. doi: 10.13700/j.bh.1001-5965.2014.0710(in Chinese)
Citation: WU Chao, WANG Haowen, JIANG Chen, et al. LADRC-based attitude decoupling control for helicopter and parameters tuning[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(11): 2085-2094. doi: 10.13700/j.bh.1001-5965.2014.0710(in Chinese)

基于LADRC的直升机姿态解耦控制及参数整定

doi: 10.13700/j.bh.1001-5965.2014.0710
基金项目: 江苏高校优势学科建设工程资助项目(PAPD)
详细信息
    作者简介:

    吴超(1983-),男,安徽巢湖人,博士研究生,wuchao_nuaa@163.com

    通讯作者:

    王浩文(1969-),男,浙江台州人,教授,bobwang@tsinghua.edu.cn,研究方向为直升机动力学、直升机结构强度及振动载荷分析.

  • 中图分类号: V212.4

LADRC-based attitude decoupling control for helicopter and parameters tuning

  • 摘要: 为满足ADS-33E-PRF所规定的飞行品质,有效克服模型外部扰动的影响,提出了一种基于线性自抗扰控制(LADRC)的直升机姿态控制策略.建立UH-60A直升机的飞行动力学模型和风模型,并进行配平计算以验证动力学模型和配平算法的准确性.在增稳反馈回路的基础上,基于单输入单输出的二阶LADRC控制器搭建了UH-60A的姿态解耦控制回路.针对ADS-33E-PRF品质要求,将控制器参数整定转变为时域与频域内的约束优化问题,结合H综合算法和最速下降算法进行了优化计算.对姿态控制器的控制效果进行了品质评估,并在大气扰动下对姿态保持控制进行了仿真,仿真和品质分析表明基于LADRC的姿态控制系统具有良好的解耦性能和抗扰性.

     

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出版历程
  • 收稿日期:  2014-11-17
  • 修回日期:  2015-02-13
  • 刊出日期:  2015-11-20

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