Unloading angular momentum for inertial actuators of a spacecraft in the pitch channel-Reference-Cited by-同舟云学术

Unloading angular momentum for inertial actuators of a spacecraft in the pitch channel

Published:2011-06 Issue:3 Volume:50 Page:483-490
ISSN:1064-2307
Container-title:Journal of Computer and Systems Sciences International
language:en
Short-container-title:J. Comput. Syst. Sci. Int.

Author:

Bogachev A. V.,Vorob’eva E. A.,Zubov N. E.,Mikrin E. A.,Misrikhanov M. Sh.,Ryabchenko V. N.,Timakov S. N.

Publisher

Pleiades Publishing Ltd

Subject

Applied Mathematics,Computer Networks and Communications,Computer Vision and Pattern Recognition,Information Systems,Theoretical Computer Science,Control and Systems Engineering,Software

Link

http://link.springer.com/content/pdf/10.1134/S1064230711030075.pdf

Reference9 articles.

1. Theoretical Basics of Design of Information-Control Spacecraft Systems, Ed. by, Mikrin E.A. (Nauka, Moscow, 2006) [in Russian].

2. N. I. Yakovlev, “Dynamics of Gravitationally Oriented Gyrostat Satellite with Damping Flywheel,” Kosm. Issl. 15(4), 511–516 (1977).

3. E. N. Tokar’, “Control Problems for Gyro-Power Stabilizers,” Kosm. Issl. 16(2), 179–187 (1978).

4. V. N. Branets, V. N. Platonov, A. V. Sumarokov, et al., “Stabilization of a Wheels Carrying Communication Satellite without Angle and Angular Velocity Sensors,” Izv. Ross. Akad. Nauk, Teor. Sist. Upr., 1 (2008), 127–137 [Comp. Syst. Sci. 47 (1), 118–128 (2008)].

5. D. V. Lebedev, “Momentum Unloading of Excessive Reaction-Wheel System of a Spacecraft,” Izv. Ross. Akad. Nauk, Teor. Sist. Upr., 1 (2008), 118–124 [Comp. Syst. Sci. 47 (4), 613–620 (2008)].

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