Abstract
The capabilities of using single-gimbal control moment gyroscopes (CMGs) for the attitude control of Earth remote sensing (ERS) satellites are studied. The situation of the incomplete spinning of CMGs used for controlling the angular motion of the satellite when these gyros have a different angular momentum is considered. Control algorithms that can be applied in this situation are proposed, and it is shown that they can be used to stabilize the satellite. Using simulation, it is shown that a satellite’s angular motion can be controlled by CMGs having different angular momenta.
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REFERENCES
V. N. Platonov, “About accuracy of an Earth remote sensing spacecraft attitude-keeping without using data from inertial sensors,” Kosm. Tekh. Tekhnol., No. 3, 33–38 (2014).
A. V. Sumarokov, “The onboard algorithm for averaging the orbital motion parameters of the international space station in the ICARUS experiment,” J. Comput. Syst. Sci. Int. 57, 273 (2018).
A. V. Sumarokov, “On pointint of high resolution camera Mountedon the International Space Station using biaxial rotating platform,” Vestn. MGTU im. N. E. Baumana, Ser. Priborostr., No. 4, 85–97 (2016).
V. N. Platonov and A. V. Sumarokov, “Studying the possibility of ensuring the stabilization accuracy characteristics of an advanced spacecraft for remote sensing of the Earth,” J. Comput. Syst. Sci. Int. 57, 655 (2018).
A. R. Mkrtychyan, N. I. Bashkeev, D. I. Akashev, et al., “Developments of JSC Research Institute of Command Instruments for motion control systems of spacecraft for remote sensing of the Earth and other purposes,” in Proceedings of the 6th International Conference on Actual Problems of Creating Space Systems for Remote Sensing of the Earth (VNIIEM, Moscow, 2018), pp. 43–45.
V. N. Platonov and A. V. Sumarokov, “Supplying for stabilization accuracy of next-generation spacecraft when conducting Earth surface area mapping,” Kosmonavt. Raketostr., No. 3, 125–132 (2017).
A. E. Bryson, Jr. and Yu-Chi Ho, Applied Optimal Control (Routledge, London, 1975).
V. V. Aleksandrov, V. G. Boltyanskii, S. S. Lemak, N. A. Parusnikov, and V. M. Tikhomirov, Optimal Motion Control (Fizmatlit, Moscow, 2005) [in Russian].
D. A. Efimov, A. V. Sumarokov, and S. N. Timakov, “On the stabilization of a communication satellite without measuring its angular velocity,” J. Comput. Syst. Sci. Int. 51, 732 (2012).
V. V. Kul’ba, E. A. Mikrin, B. V. Pavlov, and V. N. Platonov, The Theoretical Basis for the Design of Information and Control Systems of Spacecraft (Nauka, Moscow, 2006) [in Russian].
V. N. Platonov, “The law of gyro stabilizer system control,” in Proceedings of the 5th Conference of Young Specialists of the Enterprise (Energiya, Korolev, 1977), pp. 57–69.
J. W. Crenshaw, “2-Speed, a single-gimbal moment gyro attitude control system,” AIAA Pap., No. 895 (1973).
V. N. Branets, D. M. Weinberg, V. P. Werestchagin, N. N. Danilov-Nitusov, V. P. Legostaev, V. N. Platonov, U. P. Semenov, V. S. Semjchkin, B. E. Chertok, and N. N. Sheremetyevsky, “Development experience of the attitude control system using single-axis control moment gyros for long-term orbiting space stations,” Acta Astronaut. 18, 91 (1988).
E. N. Tokar’ and V. N. Platonov, “Investigation of the special surfaces of non-impact gyrodin systems,” Kosm. Issled. 16, 675–685 (1978).
E. I. Somov, S. A. Butyrin, V. N. Platonov, and A. V. Sorokin, “Control of power gyro complexes of spacecraft,” in Proceedings of the 10th SPb. International Conference on Integrated Navigation Systems (Elektropribor, St. Petersburg, 2003), pp. 278–294.
B. Wie, D. Bailey, and C. Helberg, “Rapid multitarget acquisition and pointing control of agile spacecraft,” J. Guidance, Control, Dyn. 25 (1) (2002).
V. N. Branets, V. N. Platonov, A. V. Sumarokov, and S. N. Timakov, “Stabilization of a wheels carrying communication satellite without angle and angular velocity sensors,” J. Comput. Syst. Sci. Int. 47, 118 (2008).
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This work was supported by the Russian Foundation for Basic Research, project nos. 17-08-01635 and 18-08-01379.
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Translated by A. Klimontovich
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Platonov, V.N., Sumarokov, A.V. Controlling a Satellite using Single-Gimbal Control Moment Gyroscope During Their Spinning and Braking. J. Comput. Syst. Sci. Int. 59, 289–300 (2020). https://doi.org/10.1134/S1064230720020100
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DOI: https://doi.org/10.1134/S1064230720020100