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Sensitivity-based state and parameter moving horizon estimation method for liquid propellant rocket engine

Zizhao WANG Dan WANG Hongyu CHEN Zhijiang SHAO Zhengyu SONG

中国航空学报（英文版）2025，Vol.38Issue(7)：46-60,15.

中国航空学报（英文版）2025，Vol.38Issue(7)：46-60,15.DOI:10.1016/j.cja.2024.103342

Sensitivity-based state and parameter moving horizon estimation method for liquid propellant rocket engine

Zizhao WANG ¹Dan WANG ²Hongyu CHEN ²Zhijiang SHAO ¹Zhengyu SONG³

作者信息

1. State Key Laboratory of Industrial Control Technology,College of Control Science and Engineering,Zhejiang University,Hangzhou 310027,China
2. Academy of Aerospace Propulsion Technology,Xi'an 710100,China
3. China Academy of Launch Vehicle Technology,Beijing 100076,China
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摘要

关键词

Sensitivity/Moving horizon estimation/Noise covariance estimation/Parameter estimation/Liquid propellant rocket engine

Key words

Sensitivity/Moving horizon estimation/Noise covariance estimation/Parameter estimation/Liquid propellant rocket engine

引用本文复制引用

Zizhao WANG,Dan WANG,Hongyu CHEN,Zhijiang SHAO,Zhengyu SONG..Sensitivity-based state and parameter moving horizon estimation method for liquid propellant rocket engine[J].中国航空学报（英文版）,2025,38(7):46-60,15.

基金项目

The authors would like to thank Professor Furong Gao of Hong Kong University of Science and Technology for helpful discussions on topics related to this work.This work was sup-ported by the National Natural Science Foundation of China(Nos.62120106003 and 62173301). （Nos.62120106003 and 62173301）

中国航空学报（英文版）

ISSN：1000-9361

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