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The oscillations of a satellite probe towed on an inextensible line in an inhomogeneous atmosphere

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Publication:917349
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DOI10.1016/0021-8928(88)90030-5zbMath0704.70021OpenAlexW2018920528MaRDI QIDQ917349

E. M. Shakhov

Publication date: 1988

Published in: Journal of Applied Mathematics and Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0021-8928(88)90030-5


zbMATH Keywords

aerodynamic resistanceoscillations of a low-mass satellitesatellite- pendulum


Mathematics Subject Classification ID

Orbital mechanics (70M20)


Related Items (2)

MATHEMATICAL SIMULATION OF A TETHERED SATELLITE SYSTEM MOTION WITH AN INFLATABLE SPHERICAL BALLOON DURING A SPACECRAFT ORBIT INJECTION ⋮ Speed gradient method and its applications







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