The spacecraft angular velocity estimation in the orbital stabilization mode by the results of the local vertical sensor measurements

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The original manuscript was received by the editors of “Vestnik” on 26.03.2014
Contributors
Zubov N.E. — (Eng.), Deputy Director for Science, Research and Development
Center of OAO Korolev Rocket and Space Corporation “Energiya”, Professor of
Engineering, Department of Automatic Control Systems, Bauman Moscow State Technical
University, author of over 90 publications in the field of problems of spacecraft control.
Bauman Moscow State Technical University, ul. 2-ya Baumanskaya 5, Moscow, 105005
Russian Federation.
OAO Korolev Rocket and Space Corporation “Energiya”, ul. Lenina 4a, Korolev,
Moscovskaya oblast, 141070 Russian Federation.
Mikrin E.A. — (Eng.), Member of the Russian Academy of Sciences, Head of the
Department of Automatic Control Systems, Bauman Moscow State Technical University,
First Deputy General Designer, OAO Korolev Rocket and Space Corporation “Energiya”,
author of over 150 publications in the field of problems of spacecraft control.
Bauman Moscow State Technical University, ul. 2-ya Baumanskaya 5, Moscow, 105005
Russian Federation.
OAO Korolev Rocket and Space Corporation “Energiya”, ul. Lenina 4a, Korolev,
Moscovskaya oblast, 141070 Russian Federation.
12 ISSN 0236-3933. HERALD of the BMSTU. Series “Instrument Engineering”. 2014. No. 5