Minimum control for spacecraft formations in a J2 perturbed environment

DOI10.1007/S10569-009-9214-5zbMath1223.70096OpenAlexW2019476106WikidataQ59196871 ScholiaQ59196871MaRDI QIDQ642303

G. B. Palmerini, Dario Izzo, Sabatini, Marco

Publication date: 26 October 2011

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

Full work available at URL: https://doi.org/10.1007/s10569-009-9214-5

zbMATH Keywords

formation flyingmagic inclinationsorbital controlprojected circular orbit (PCO)quasi-PCO orbits

Mathematics Subject Classification ID

Control of mechanical systems (70Q05) Orbital mechanics (70M20)

Related Items (2)

Application of Hamiltonian structure-preserving control to formation flying on a \(J_2\)-perturbed mean circular orbit ⋮ Improved initialization conditions and single impulsive maneuvers for \(J_2\)-invariant relative orbits

Cites Work

• Second-order state transition for relative motion near perturbed, elliptic orbits
• Modelling natural formations of LEO satellites
• An intelligent control concept for formation flying satellites

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