Orbital perturbations due to radiation pressure for a spacecraft of complex shape

DOI10.1007/BF01358596zbMath0512.70030MaRDI QIDQ3657504

A. M. Nobili, Bruno Bertotti, L. Anselmo, Paolo Farinella, Andrea Milani

Publication date: 1983

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

zbMATH Keywords

perturbationeccentricityradiation pressurecylindrical symmetrylongitudeinclinationforce acting on spacecrafthigh orbitlong- time satelliteslong-period effects on semimajor axisthermo-optical properties

Mathematics Subject Classification ID

Astronomy and astrophysics (85A99) Orbital mechanics (70M20) Control/observation systems governed by ordinary differential equations (93C15)

Related Items (9)

A numerical solution for LAGEOS thermal thrust: The rapid-spin case ⋮ Earth albedo and the orbit of Lageos ⋮ Sensitivity of LAGEOS to changes in Earth's (2, 2) gravity coefficients ⋮ Investigation of the effect of albedo and oblateness on the circular restricted four variable bodies problem ⋮ COORBITAL RESTRICTED PROBLEM AND ITS APPLICATION IN THE DESIGN OF THE ORBITS OF THE LISA SPACECRAFT ⋮ METHODS FOR ORBIT OPTIMIZATION FOR THE LISA GRAVITATIONAL WAVE OBSERVATORY ⋮ The equations of motion of the joint effects of the relativistic and solar radiation pressure on an Earth artificial satellite. ⋮ Modeling of the radial and transverse components of the albedo function ⋮ The relativistic and direct solar radiation pressure effects on an axially symmetric spacecraft. I: The Hamiltonian and the canonical equations of motion.

Cites Work

• Short-period and long-period perturbations of a spherical satellite due to direct solar radiation

This page was built for publication: Orbital perturbations due to radiation pressure for a spacecraft of complex shape