基于线性自抗扰控制技术控制器设计的控制方法
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V233.75

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大飞机重大专项


Study on Control method for Designing Set-Point Controller via LADRC Technique
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    摘要:

    为实现无超调、无偏差且快速的风扇转速设定点控制。利用线性自抗扰控制(LADRC)技术设计设定点控制器,并将控制器进行参数整定,应用于风扇转速设定点控制中。一方面,线性扩张状态观测器(LESO)存在于LADRC中,从而具有在大范围内很好地补偿参数波动对系统输出的影响,提高了系统的控制精度与响应速度。另一方面,为突出LADRC优良控制性能,对比经典的发动机控制方法,将各方法所设计的控制器应用于风扇转速设定点控制中。仿真结果表明:在两种完全不同飞行条件下的发动机模型中,只有LADRC控制器依旧满足优异的性能,其控制输出依旧满足稳态偏差为零、无超调且调节时间小于1秒。

    Abstract:

    In order to meet no overshoot, no deviation and fast set-point control via fan speed. The linear active disturbance rejection control (LADRC) technique was used for designing the set-point controller, and the appropriate parameters that the LADRC controller were selected by parameter adjustment for the set-point control of fan speed. On the one hand, due to the existence of the linear extended state observer (LESO) in LADRC, the influence of parameter fluctuation on the system output could been compensated in a large range, so the control precision and response speed of the system are improved. On the other hand, LADRC controller had a comparison with other controllers that were designed by classical control methods of engine, in order to show its performances. The simulation shows that the LADRC controller is applied to two engine models under completely different flight conditions. The control output still meets the steady-state deviation of zero, not overshoot and the adjustment time is less than 1 second.

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白杰,朱日兴,王伟,等. 基于线性自抗扰控制技术控制器设计的控制方法[J]. 科学技术与工程, 2020, 20(10): 4149-4153.
Bai Jie, Zhu Rixing, Wang Wei, et al. Study on Control method for Designing Set-Point Controller via LADRC Technique[J]. Science Technology and Engineering,2020,20(10):4149-4153.

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历史
  • 收稿日期:2019-07-20
  • 最后修改日期:2019-11-27
  • 录用日期:2019-09-25
  • 在线发布日期: 2020-05-19
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