Higher-order analytical attitude propagation of an oblate rigid body under gravity-gradient torque

DOI10.1155/2012/123138zbMath1264.70058OpenAlexW2076352230WikidataQ58912446 ScholiaQ58912446MaRDI QIDQ1954454

Yanyan Li

Publication date: 11 June 2013

Published in: Mathematical Problems in Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1155/2012/123138

Mathematics Subject Classification ID

Orbital mechanics (70M20) Averaging of perturbations for nonlinear problems in mechanics (70K65)

Related Items (1)

Semianalytic integration of high-altitude orbits under lunisolar effects

Cites Work

• Spin-stabilized spacecrafts: analytical attitude propagation using magnetic torques
• Analytical and semi-analytical analysis of an artificial satellite's rotational motion
• On the effect of the mantle elasticity on the Earth's rotation
• New canonical variables for orbital and rotational motions
• Study of the terms of coupling between rotational and translational motions
• First-order rotation solution of an oblate rigid body under the torque of a perturber in circular orbit
• On the motion of a satellite about its center of mass under the action of gravitational moments
• Gravity effects on the rotational motion of a uniaxial artificial satellite.
• Canonical transformations depending on a small parameter
• Equivalence of the perturbation theories of Hori and Deprit
• Effects of gravity-gradient torque on the rotational motion of A triaxial satellite in a precessing elliptic orbit

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