Phase compensation active disturbance rejection control for shimmy vibration with magnetorheological damper of aircraft

Author:

Dong Lei,Chen ZengqiangORCID,Sun Mingwei,Sun Qinglin

Funder

National Natural Science Foundation of China

Natural Science Foundation of Tianjin City

Tianjin Research Innovation Project for Postgraduate Students

Publisher

Elsevier BV

Subject

Artificial Intelligence,Computer Science Applications,General Engineering

Reference31 articles.

1. Parameterized fuzzy-logic controllers for the attitude control of nanosatellites in low earth orbits. a comparative studio with pid controllers;Bello;Expert Systems with Applications,2021

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3. A hysteresis model for the field-dependent damping force of a magnetorheological damper;Choi;Journal of Sound and Vibration,2001

4. Some aspects of nose-wheel shimmy and shimmy damper of the aircraft;Chu;Acta Aeronautica et Astronautica Sinica,1981

5. The active damper: a new concept for shock and vibration control;Crosby;Shock and Vibration Bulletin,1973

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