New State Transition Matrices for Spacecraft Relative Motion in Perturbed Orbits

@article{Koenig2017NewST,
  title={New State Transition Matrices for Spacecraft Relative Motion in Perturbed Orbits},
  author={Adam W. Koenig and Tommaso Guffanti and Simone D’Amico},
  journal={Journal of Guidance Control and Dynamics},
  year={2017},
  volume={40},
  pages={1749-1768}
}
This paper presents new state transition matrices that model the relative motion of two spacecraft in arbitrarily eccentric orbits perturbed by J2 and differential drag for three state definitions ... 

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