Моделирование демпфирования углового движения наноспутника с помощью гистерезисной пластины

DOI10.20948/MM-2020-02-06zbMath1439.78010OpenAlexW3005636000MaRDI QIDQ5112275

V. I. Pen'kov, Tatiana A. Ivanova, D. S. Ivanov, Michael Ovchinnikov

Publication date: 29 May 2020

Published in: Математическое моделирование (Search for Journal in Brave)

Full work available at URL: http://mathnet.ru/eng/mm4157

zbMATH Keywords

angular motionnanosatellitehysteresis damper

Mathematics Subject Classification ID

Controllability (93B05) Kinematics of a rigid body (70B10) Control of mechanical systems (70Q05) Technical applications of optics and electromagnetic theory (78A55) Electro- and magnetostatics (78A30) Problems involving hysteresis in solids (74N30)

Related Items (1)

Nonlinear control with distributed delay for the angular stabilization of a rigid body

Cites Work

• Attitude control of a rigid body suspended by string with the use of ventilator engines
• Laboratory study of magnetic properties of hysteresis rods for attitude control systems of minisatellites
• A laboratory facility for verification of control algorithms for a group of satellites
• Laboratory facility for microsatellite mock-up motion simulation
• Testing of attitude control algorithms for microsatellite ``Chibis-M at laboratory facility

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