E/I-vector separation for safe switching of the GRACE formation

DOI10.1016/j.ast.2006.04.001zbMath1195.70039OpenAlexW2039863652MaRDI QIDQ4929524

Simone D'Amico, Oliver Montenbruck, Michael Kirschner, Srinivas Bettadpur

Publication date: 23 September 2010

Published in: Aerospace Science and Technology (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.ast.2006.04.001

zbMATH Keywords

formation flyingGRACEE/I-vector separationproximity operations

Mathematics Subject Classification ID

Orbital mechanics (70M20)

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The Hamiltonian structure-preserving control and some applications to nonlinear astrodynamics ⋮ Formation dynamics in geostationary ring ⋮ Equilibrium configurations of the tethered three-body formation system and their nonlinear dynamics ⋮ Application of Hamiltonian structure-preserving control to formation flying on a \(J_2\)-perturbed mean circular orbit ⋮ Bounded motion design in the Earth zonal problem using differential algebra based normal form methods

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