COMPENSATION OF THE REACTION MOMENT IN ELECTRIC DRIVE OF SATELLITE ON BOARD SYSTEMS
ARTICLE_8_PDF (Українська)

Keywords

satellite
electric drive
torke
reaction torque спутник
электропривод
момент вращения
реактивный момент

How to Cite

[1]
Антонов, А., Акинін, К. and Киреев, В. 2018. COMPENSATION OF THE REACTION MOMENT IN ELECTRIC DRIVE OF SATELLITE ON BOARD SYSTEMS. Tekhnichna Elektrodynamika. 3 (May 2018), 066. DOI:https://doi.org/10.15407/techned2018.03.066.

Abstract

The peculiarities of the construction of an electric drive stabilized by speed, which operates as part of an autonomous spacecraft, are considered. To prevent the negative action of the reaction torque of the engine rotating which rotates the satellite in the opposite directionthe satellite it is proposed coaxial with the drive motor to install an adjustable compensating motor, which creates a torque of the opposite sign. An algorithm for controlling the drive and compensating motors is proposed. The possible change in the bearing's resistance moment is considered, which in the conditions of space is the only source of the torque of the engine.  References 8, figures 7, table 1.

https://doi.org/10.15407/techned2018.03.066
ARTICLE_8_PDF (Українська)

References

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Gyroscopic systems. Part. 3. Moskva: Vysshaia shkola, 1972. 242 p. (Rus)

Gyroscopes. Production and research. Moskva: Mashinostroenie, 1969. P. 134-156. (Rus)

Mikhailov E.M. The frictional moment in ball bearings for spacecraft. Voprosy elektromekhaniki. 2014. Vol. 140. P. 3-6. (Rus)

Basics of designing servo systems. Moskva: Mashinostroenie, 1978. 391 p. (Rus)

Device ball-shaped bearings. Spravochnik. Moskva: Energiia, 1981. 75 p. (Rus)

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