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Updated: Sep 19, 2025

Design and Application of a Fault Detection Method Based on Adaptive Filters and Rotational Speed Estimation for an Electro-Hydrostatic Actuator
06:45

Design and Application of a Fault Detection Method Based on Adaptive Filters and Rotational Speed Estimation for an Electro-Hydrostatic Actuator

Published on: October 28, 2022

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一种基于数据的在线估计方法,用于高速飞机的空气动力学参数,考虑到强烈的非线性和噪声

Bowen Xu1, Weiqi Yang1, Yunfan Zhou1

  • 1Advanced Propulsion Technology Laboratory, National University of Defense Technology, Changsha, China.

ISA transactions
|May 30, 2025
PubMed
概括

本研究介绍了一种使用最小正方形支向量机 (LS-SVM) 和无气味卡尔曼波器 (UKF) 的在线建模方法,用于在复杂的机动中准确估计高速飞机的空气动力学参数.

关键词:
航空动力学参数 航空动力学参数高速度飞机飞机的飞行器.非线性模型是一种非线性模型.在线估计在线估计参数识别 参数识别

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