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The effect of external perturbing moments on the dynamics of a uniaxial single-flywheel attitude control system of a spacecraft: PMM vol. 31, no. 6, 1967, pp. 1095–1103

✍ Scribed by A.A. Karymov; T.V. Kharitonova


Publisher
Elsevier Science
Year
1967
Tongue
English
Weight
670 KB
Volume
31
Category
Article
ISSN
0021-8928

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