Orbit covariance propagation via quadratic-order state transition matrix in curvilinear coordinates

DOI10.1007/S10569-017-9773-9zbMath1375.70072OpenAlexW2724801566MaRDI QIDQ1682191

Javier Hernando-Ayuso, Claudio Bombardelli

Publication date: 28 November 2017

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

Full work available at URL: https://doi.org/10.1007/s10569-017-9773-9

zbMATH Keywords

curvilinear coordinatesstate transition matrixClohessy-Wiltshire solutionquadratic solutionorbit uncertainty

Mathematics Subject Classification ID

Orbital mechanics (70M20)

Related Items (1)

The circular restricted three-body problem in curvilinear coordinates

Cites Work

• Unnamed Item
• Approximate solutions of non-linear circular orbit relative motion in curvilinear coordinates

This page was built for publication: Orbit covariance propagation via quadratic-order state transition matrix in curvilinear coordinates