Inverse Transformation of Elliptical Relative State Transition Matrix

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References

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http://dx.doi.org/10.1007/BF00692510

[2] Garrison, J.L., Gardner, J.L. and Axelrad, P. (1995) Relative Motion in Highly Elliptical Orbits. Paper No. AAS 95-194, Space Flight Mechanics Conference, Alburquerque.

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[4] Gim, D.-W. and Alfriend, K.T. (2005) Satellite Relative Motion Using Differential Equinoctial Elements. Celestial Mechanics and Dynamical Astronomy, 92, 295-336. http://dx.doi.org/10.1007/s10569-004-1799-0

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http://dx.doi.org/10.1007/s10569-006-9054-5

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[9] Han, C. and Yin, J. (2012) Formation Design in Elliptical Orbit Using Relative Orbit Elements. Acta Astronautica, 77, 34-47. http://dx.doi.org/10.1016/j.actaastro.2012.02.026

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http://dx.doi.org/10.2514/1.13173