A novel ADRC-based design for a kind of flexible aerocraft
Sheng Zhong1
Yi Huang1
Sen Chen2
Lin Dai3
1.Key Laboratory of Systems and Control,Academy of Mathematics and Systems Science,Chinese Academy of Sciences,Beijing 100190,China;School of Mathematical Sciences,University of Chinese Academy of Sciences,Beijing 100049,China2.School of Mathematics and Information Science,Shaanxi Normal University,Xi'an,Shaanxi 710119,China3.Beijing System Design Institute of Electro-Mechanic Engineering,Beijing 100854,China
摘要:The paper presents a novel control design,which is based on the idea of active disturbance rejection control(ADRC),for a kind of flexible aerocraft whose controlled variable cannot be measured directly.Since the original frame of ADRC can-not be directly applied,the paper puts forward a new extended state observer(ESO)and the corresponding ADRC law.In order to assign the poles of the closed-loop system to ideal positions such that the vibration can be quickly suppressed,an elastic damping term is added into feedback law.The advantages of the new ESO for effectively estimating both the rigid mode and elastic mode from the measurements are discussed.Moreover,the analysis on the stability,the relative stability and the steady state of the closed-loop system is given.Finally,the effectiveness and robustness of the proposed ADRC are verified by simulations.
机标关键词:
论文发表日期:2021-02-05
在线出版日期:2025-08-15(本平台首次上网日期,不代表文献的发表时间)
页数:14( 35-48 )
英文信息
