Energy preserving low-thrust guidance for orbit transfers in KS variables

Author:

Hernandez Sonia,Akella Maruthi R.

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Astronomy and Astrophysics,Applied Mathematics,Computational Mathematics,Mathematical Physics,Modelling and Simulation

Reference25 articles.

1. Aarseth, S.J.: Gravitational N-Body Simulations. Cambridge University Press, Cambridge (2003)

2. Battin, R.H.: An introduction to the mathematics and methods of astrodynamics. In: AIAA Education Series, p. 182, 489 (1999)

3. Berry, M.M., Healy, L.M.: The generalized sundman transformation for propagation of high-eccentricity elliptical orbits. In: AAS/AIAA Space Flight Mechanics Meeting, AAS 02–109, San Antonio, Texas (2002)

4. Bettis, D.G., Szebehely, V.: Treatment of close approaches in the numerical implementation integration of the gravitational problem of n bodies. Astrophys. Space Sci. 14(1), 133–150 (1971)

5. Chang, D.E., Chichka, D.F., Marsden, J.E.: Lyapunov-based transfer between elliptic keplerian orbits. Discrete Contin. Dyn. Syst. Ser. B 2(1), 57–67 (2002)

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