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[2] Zubov N.E. Optimal control of spacecraft terminal orientation on the basis of an

algorithm with a predicting model.

Cosmic Res.

, vol. 29, no. 3, pp. 340–350 (in

Russ.).

[3] Krasovskiy A.A., ed. Handbook of Automatic Control Theory. Moscow, Nauka Publ.,

1987.

[4] Zubov N.E., Mikrin E.A., Misrikhanov

M.Sh

., Ryabchenko V.N., Timakov S.N.,

Cheremnykh E.A. Identification of the Position of an Equilibrium Attitude of the

International Space Station as a Problem of Stable Matrix Completion.

J. Computer

and Systems Sciences International

, 2012, vol. 51, pp. 291–305.

[5] Zubov N.E., Mikrin E.A., Ryabchenko V.N., et al. The Use of an Adaptive Bandpass

Filter as an Observer in the Control Loop of the International Space Station.

J.

Computer and Systems Sciences International

, 2012, vol. 51, pp. 560–572.

[6] Zubov N.E., Mikrin E.A., Misrikhanov

M.Sh

., Ryabchenko V.N., Timakov S.N. The

Use of the Exact Pole Placement Algorithm for the Control of Spacecraft Motion.

J.

Computer and Systems Sciences International

, 2013, vol. 52, pp. 129–144.

[7] Zubov N.E., Vorob’eva E.A., Mikrin E.A., Misrikhanov

M.Sh

., Ryabchenko V.N.,

Timakov S.N. Synthesis of Stabilizing Spacecraft Control Based on Generalized

Ackermann’s Formula.

J. of Computer and Systems Sciences International

, 2011,

vol. 50, pp. 93–103.

[8] Bogachev A.V., Vorob’eva E.A., Zubov N.E., Mikrin E.A., Misrikhanov

M.Sh

.,

Ryabchenko V.N., Timakov S.N. Unloading Angular Momentum for Inertial

Actuators of a Spacecraft in the Pitch Channe.

J. Computer and Systems Sciences

International

, 2011, vol. 50, pp. 483–490.

[9] Zubov N.E., Mikrin E.A., Misrikhanov

M.Sh

., Ryabchenko V.N. Synthesis of

decoupling laws for attitude stabilization of a spacecraft.

J. Computer and Systems

Sciences International

, 2012, vol. 51, pp. 80–96.

[10] Zubov N.E., Mikrin E.A., Misrikhanov

M.Sh

., Ryabchenko V.N. Modification the

Exact Pole Placement Method and its Application for the Control of Spacecraft

Motion.

J. of Computer and Systems Sciences International

, 2013, vol. 52, pp. 279–

292.

[11] Zubov N.E., Mikrin E.A., Misrikhanov

M.Sh

., and Ryabchenko V.N. Synthesis of

Controls for a Spacecraft that Optimize the Pole Placement of the Closed Loop

Control System.

J. Computer and Systems Sciences International

, 2012, vol. 51,

pp. 431–444.

[12] Zubov N.E., Mikrin E.A., Oleinik A.S., Ryabchenko V.N., Efanov D.E. The

spacecraft angular velocity estimation in the orbital stabilization mode by the

results of the local vertical sensor measurements.

Vestn. Mosk. Gos. Tekh. Univ.

im. N.E. Baumana, Priborostr.

[Herald of the Bauman Moscow State Tech. Univ.,

Instrum. Eng.], 2014, no. 5, pp. 3–15 (in Russ.).

[13] Zubov N.E., Mikrin E.A., Misrikhanov

M.Sh

., Oleinik A.S., Ryabchenko V.N.

Terminal bang-bang impulsive control of linear time invariant dynamic systems.

J. Comput. Syst. Sci. Int

., 2014, vol., 53, pp. 480–490.

Статья поступила в редакцию 5.02.2015

Зубов Николай Евгеньевич — д-р техн. наук, заместитель руководителя по науке

научно-технического центра ОАО “РКК “Энергия” им. С.П. Корол¨eва”, профессор

кафедры “Системы автоматического управления” МГТУ им. Н.Э. Баумана.

ОАО “РКК “Энергия” им. С.П. Корол¨eва”, Российская Федерация, 141070, Москов-

ская обл., г. Корол¨eв, ул. Ленина, д. 4-а.

МГТУ им. Н.Э. Баумана, Российская Федерация, 105005, Москва, 2-я Бауманская ул.,

д. 5.

18 ISSN 0236-3933. Вестник МГТУ им. Н.Э. Баумана. Сер. “Приборостроение”. 2015. № 6