State Transition Matrix of Relative Motion for the Perturbed Noncircular Reference Orbit
By Dong-Woo Gim, K. Alfriend. 2003
450 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Astronomy and Astrophysics
View Paper: https://www.semanticscholar.org/paper/284fddd92b9714448993527a03505e2459541e76
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In Aerospace Engineering
- Soon-Jo Chung
- Lars Blackmore
- Simone D'Amico
- Joshua Sullivan
- Fred Y. Hadaegh
- Behçet Açikmese
- Xinfu Liu
- Ping Lu
In Astronomy and Astrophysics
Citations in the corpus
- Swarm-Keeping Strategies for Spacecraft Under J2 and Atmospheric Drag Perturbations (2011, methodology): “Gim and Alfriend [19] derived the relative dynamics in the form of a state transitionmatrix.”
- Nonlinear Kalman Filtering for Improved Angles-Only Navigation Using Relative Orbital Elements (2017, methodology): “As an interesting illustration, one might attempt to confront the observability problem of angles-only estimation using the Gim– Alfriend dynamics model [30,31], which captures the evolution of the mean OED subject to secular J2 perturbation effects in arbitrarily eccentric orbits, and subsequently ”