Gravitational orbit-attitude coupling for very large spacecraft

DOI10.1007/BF01686816zbMath0549.70020OpenAlexW2058164931MaRDI QIDQ3341981

P. C. Hughes, G. B. Sincarsin

Publication date: 1983

Published in: Celestial Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf01686816

zbMATH Keywords

computer simulation of orbit-attitude (coupled) motionhigher moments of inertia

Mathematics Subject Classification ID

Computational methods for problems pertaining to mechanics of particles and systems (70-08) Astronomy and astrophysics (85A99) Orbital mechanics (70M20) Dynamics of a rigid body and of multibody systems (70E99)

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Generating function of the inertial integrals for small celestial bodies, Dynamic limits on planar libration-orbit coupling around an oblate primary, Inertial Characteristics of Higher Orders and Dynamics in a Proximity of a Small Celestial Body, Hamiltonian dynamics of a rigid body in a central gravitational field, Hamiltonian structure and relative equilibria of an axisymmetric rigid body in a second degree and order gravity field: cylindrical and generalized hyperbolic equilibria, Orbital dynamics and equilibrium points around an asteroid with gravitational orbit-attitude coupling perturbation

Cites Work

• Stability of a spinning body containing elastic parts via Liapunov'sdirect method
• Interaction between attitude libration and orbital motion of a rigid body in a near keplerian orbit of low eccentricity