首页|A novel ADRC-based design for a kind of flexible aerocraft
A novel ADRC-based design for a kind of flexible aerocraft
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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.
Attitude control for flexible aerocraftActive disturbance rejection control(ADRC)Extended state observer(ESO)
Sheng Zhong、Yi Huang、Sen Chen、Lin Dai
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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,China
School of Mathematics and Information Science,Shaanxi Normal University,Xi'an,Shaanxi 710119,China
Beijing System Design Institute of Electro-Mechanic Engineering,Beijing 100854,China
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This work was supported by the National Key R&D Program of ChinaNational Center for Mathematics and Interdisciplinary Sciences,Chinese Acad-emy of Sciences
NETL
NSTL
万方数据
维普
