Applications of multi-body dynamical environments: The ARTEMIS transfer trajectory design

Author:

Folta David C.,Woodard Mark,Howell Kathleen,Patterson Chris,Schlei Wayne

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference32 articles.

1. D. Folta, F. Vaughn. A survey of Earth–Moon libration orbits: stationkeeping strategies and intra-orbit transfers, Paper no. IAC-02-Q.6.08, in: Proceedings of the 53rd International Astronautical Congress, World Space Congress, Houston, TX, USA, October 10–19, 2002.

2. K.C. Howell, B.T. Barden, R.S. Wilson, M.W. Lo, Trajectory design using a dynamical systems approach with application to GENESIS, AAS/AIAA Astrodynamics 1997, Advances in the Astronautical Sciences, vol. 97, Part II, F. Hoots, B. Kaufman, P. Cefola, D. Spencer (Eds.), 1997, pp. 1665–1684.

3. Orbit determination error analysis and a station-keeping strategy for Sun –Earth L1 libration point orbits;Howell;J. Astronaut. Sci.,1994

4. Dynamics and Mission Design Near Libration Points, I: Fundamentals: The Case of Collinear Libration Points;Gómez,2001

5. Connecting orbits and invariant manifolds in the spatial restricted three-body problem;Gómez;Nonlinearity,2004

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