First-order theory of satellite attitude motion application to HIPPARCOS

DOI10.1007/BF01230479zbMath0614.70027OpenAlexW2032315273MaRDI QIDQ4721700

Eric Bois

Publication date: 1986

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

Full work available at URL: https://doi.org/10.1007/bf01230479

zbMATH Keywords

numerical integrationanalytic solutionposition of equilibriumdisturbing torquesHIPPARCOS modelattitude evolutionperturbed rotation satellitesolar radiation pressure torque

Mathematics Subject Classification ID

Computational methods for problems pertaining to mechanics of particles and systems (70-08) Orbital mechanics (70M20)

Related Items (2)

First-order accurate theory of perturbed circular motion ⋮ Second-order theory of the rotation of an artificial satellite

Cites Work

• Perturbation solution of attitude motion under body-fixed torques
• Gravity effects on the rotational motion of a uniaxial artificial satellite.
• Rotational equations of motion for a triaxial rigid body
• [https://portal.mardi4nfdi.de/wiki/Publication:5661193 Influence du champ magn�tique terrestre sur le mouvement d'un satellite autour de son centre de gravit�]

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