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热真空试验中的自校正PID控制策略
引用本文:孙宇,刘高同,顾志飞,詹海洋.热真空试验中的自校正PID控制策略[J].航天器环境工程,2016,33(3):333-336.
作者姓名:孙宇  刘高同  顾志飞  詹海洋
作者单位:北京卫星环境工程研究所, 北京 100094
摘    要:通过引入自校正PID控制策略解决热真空试验温度调节过程中存在的长滞后问题。首先,采用带遗忘因子的递推最小二乘法对未知模型的特征参数进行在线辨识;然后,进行自校正PID的控制律设计。仿真结果表明:该方法可以比较准确地辨识出模型特征参数;与传统的PID控制方法相比,具有响应速度较快、超调量较小等优点。

关 键 词:热真空试验  系统辨识  最小二乘法  自校正PID
收稿时间:2015/10/29 0:00:00
修稿时间:2016/5/23 0:00:00

Self-tuning PID control strategy for thermal vacuum tests
Sun Yu,Liu Gaotong,Gu Zhifei,Zhan Haiyang.Self-tuning PID control strategy for thermal vacuum tests[J].Spacecraft Environment Engineering,2016,33(3):333-336.
Authors:Sun Yu  Liu Gaotong  Gu Zhifei  Zhan Haiyang
Institution:Beijing Institute of Spacecraft Environment Engineering, Beijing 100094, China
Abstract:A self-tuning PID control strategy is adopted for the temperature control problem with long time delays. First, the recursive least square method is used with a forgetting factor to identify on line the unknown characteristic parameters of the model. Then, a self-tuning PID control law is designed. The simulation results show that this method can accurately identify the characteristic parameters of the model and the self-tuning PID approach boasts faster response and smaller overshoot than the conventional PID control method.
Keywords:thermal vacuum tests  system identification  least square method  adaptive PID
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