Modeling orbital relative motion to enable formation design from application requirements

DOI10.1007/s10569-009-9230-5zbMath1223.70083OpenAlexW2093751015MaRDI QIDQ642301

Giancarmine Fasano, Marco D'errico

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/s10569-009-9230-5

zbMATH Keywords

formation flyingrelative dynamicsrelative trajectory designtime-explicit analytical model

Mathematics Subject Classification ID

Orbital mechanics (70M20)

Related Items (5)

A new family of multistep numerical integration methods based on Hermite interpolation ⋮ A second-order solution to the two-point boundary value problem for rendezvous in eccentric orbits ⋮ Relative motion of satellites exploiting the super-integrability of Kepler's problem ⋮ Time-varying transformations for Hill-Clohessy-Wiltshire solutions in elliptic orbits ⋮ Frozen-anomaly transformation for the elliptic rendezvous problem

Cites Work

• Unnamed Item
• Satellite relative motion using differential equinoctial elements
• Second-order state transition for relative motion near perturbed, elliptic orbits
• Modelling natural formations of LEO satellites
• Analysis of spaceborne tandem configurations for complementing COSMO with SAR interferometry
• State Transition Matrices for Terminal Rendezvous Studies: Brief Survey and New Example
• Synthetic aperture radar interferometry
• \(J_2\) invariant relative orbits for spacecraft formations

This page was built for publication: Modeling orbital relative motion to enable formation design from application requirements