Stability of large flexible damped spacecraft modeled as elastic continua

DOI10.1016/0094-5765(84)90002-XzbMath0535.73043OpenAlexW2054508574MaRDI QIDQ3319874

Shashi K. Shrivastava, Prashant K. Maharana

Publication date: 1984

Published in: Acta Astronautica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0094-5765(84)90002-x

zbMATH Keywords

Floquet theorymodal analysisspinningelastic continuumcritical dampingvibrational stabilitylarge rigid body rotationsfunction of the spacecraft's inertia ratio and the level of disturbancelarge flexible, structurally damped spacecraftnon-spinningordinary differential equations with time-varying coefficientsrigid body attitude motionSonin-Polya theoremspacecraft idealized as a flexible beam/platetorque free conditions

Mathematics Subject Classification ID

Vibrations in dynamical problems in solid mechanics (74H45) Stability theory for ordinary differential equations (34D99)

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