High-Fidelity Linearized J Model for Satellite Formation Flight
By S. Schweighart, R. Sedwick. 2002
415 citations recorded by the source corpus.
View Paper: https://www.semanticscholar.org/paper/6f42b54d39a6c011487f8c970f39953c5550780d
How researchers see this paper
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- Marcello Romano
- R. Bevilacqua
Citations in the corpus
- Rendezvous Maneuvers of Multiple Spacecraft Using Differential Drag Under J2 Perturbation (2008, methodology): “The linearized dynamicmodel of a spacecraft movingwith respect to a circular orbit, including the J2 effects, as introduced by Schweighart and Sedwick in [11], is 1596 BEVILACQUA AND ROMANO”