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热真空试验中的自校正PID控制策略

孙宇 刘高同 顾志飞 詹海洋

航天器环境工程2016,Vol.33Issue(3):333-336,4.
航天器环境工程2016,Vol.33Issue(3):333-336,4.DOI:10.3969/j.issn.1673-1379.2016.03.018

热真空试验中的自校正PID控制策略

Self-tuning PID control strategy for thermal vacuum tests

孙宇 1刘高同 1顾志飞 1詹海洋1

作者信息

  • 1. 北京卫星环境工程研究所,北京 100094
  • 折叠

摘要

Abstract

Aself-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.

关键词

热真空试验/系统辨识/最小二乘法/自校正PID

Key words

thermal vacuum tests/system identification/least square method/adaptive PID

分类

信息技术与安全科学

引用本文复制引用

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):333-336,4.

航天器环境工程

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1673-1379

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