Search Results - "Penkov, V.I."

Geomagnetic field models for satellite angular motion studies by Ovchinnikov, M. Yu, Penkov, V.I., Roldugin, D.S., Pichuzhkina, A.V.

“…Four geomagnetic field models are discussed: IGRF, inclined, direct and simplified dipoles. Geomagnetic induction vector expressions are provided in different…”
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Three-axis active magnetic attitude control asymptotical study by Ovchinnikov, M.Yu, Roldugin, D.S., Penkov, V.I.

“…Active magnetic attitude control system providing given inertial attitude is considered. Control algorithm is constructed on the basis of a planar motion…”
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Advanced numerical study of the three-axis magnetic attitude control and determination with uncertainties by Ivanov, D.S., Ovchinnikov, M.Yu, Penkov, V.I., Roldugin, D.S., Doronin, D.M., Ovchinnikov, A.V.

“…Attitude motion of a satellite equipped with magnetic control system is considered. System comprises of three magnetorquers and one three-axis magnetometer…”
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Single axis stabilization of a fast rotating satellite in the orbital frame using magnetorquers and a rotor by Ovchinnikov, M. Yu, Penkov, V.I., Roldugin, D.S., Tkachev, S.S.

“…Fast rotating satellite with a rotor is considered. Overall angular momentum of the satellite-rotor system is small. Satellite rotation rate is determined by…”
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B-dot algorithm steady-state motion performance by Ovchinnikov, M. Yu, Roldugin, D.S., Tkachev, S.S., Penkov, V.I.

“…Satellite attitude motion subject to the well-known B-dot magnetic control is considered. Unlike the majority of studies the present work focuses on the slowly…”
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Fully magnetic sliding mode control for acquiring three-axis attitude by Ovchinnikov, M.Yu, Roldugin, D.S., Penkov, V.I., Tkachev, S.S., Mashtakov, Y.V.

“…Satellite equipped with purely magnetic attitude control system is considered. Sliding mode control is used to achieve three-axis satellite attitude…”
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Choosing control parameters for three axis magnetic stabilization in orbital frame by Ovchinnikov, M.Yu, Roldugin, D.S., Ivanov, D.S., Penkov, V.I.

“…Three-axis magnetic control in orbital reference frame is considered. Magnetorquers are the only actuators and gravitational torque is the only disturbance…”
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Asymptotic study of a complete magnetic attitude control cycle providing a single-axis orientation by Ovchinnikov, M.Yu, Roldugin, D.S., Penkov, V.I.

“…The angular motion of an axisymmetrical satellite equipped with the active magnetic attitude control system is examined. Attitude control system has to ensure…”
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Attitude dynamics of the first Russian nanosatellite TNS-0 by Ovchinnikov, M.Yu, Ilyin, A.A., Kupriynova, N.V., Penkov, V.I., Selivanov, A.S.

“…Attitude dynamics of the first Russian nanosatellite TNS-0 is considered. The satellite is equipped with an attitude control system comprising a strong…”
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