Satellite relative motion using differential equinoctial elements

DOI10.1007/s10569-004-1799-0zbMath1129.70331OpenAlexW1987711364MaRDI QIDQ816888

Dong-Woo Gim, Kyle T. Alfriend

Publication date: 2 March 2006

Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10569-004-1799-0

zbMATH Keywords

relative motiongeometric methodstate transition matrixequinoctial variables

Mathematics Subject Classification ID

Celestial mechanics (70F15) Orbital mechanics (70M20)

Related Items (13)

Integrable approximation of \(J_2\)-perturbed relative orbits ⋮ Solutions and periodicity of satellite relative motion under even zonal harmonics perturbations ⋮ A satellite relative motion model including \(J_2\) and \(J_3\) via Vinti's intermediary ⋮ Second-order state transition for relative motion near perturbed, elliptic orbits ⋮ Сравнение моделей относительного движения группы космических аппаратов ⋮ Approximate analysis for relative motion of satellite formation flying in elliptical orbits ⋮ The theory of asynchronous relative motion. I: Time transformations and nonlinear corrections ⋮ Nonlinear analytic solution for perturbed relative motion using differential equinoctial elements ⋮ Modeling orbital relative motion to enable formation design from application requirements ⋮ Modelling natural formations of LEO satellites ⋮ On a set of \(J_2\) equinoctial orbital elements and their use for uncertainty propagation ⋮ Frozen-anomaly transformation for the elliptic rendezvous problem ⋮ The relative motion of earth orbiting satellites

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