Analysis of Fuel Consumption to Maintain the Formation of Four Satellites in a Circular Configuration

Author:

Danhe Chen ,Baranov A. A.,Chernov N. V.

Publisher

Pleiades Publishing Ltd

Subject

Space and Planetary Science,Astronomy and Astrophysics,Aerospace Engineering

Reference17 articles.

1. Marec, J.-P., Optimal space trajectories, Studies in Astronautics, Amsterdam: Elsevier, 1979, vol. 1.

2. Jones, J.B., Optimal rendezvous in the neighborhood of a circular orbit, J. Astronaut. Sci., 1976, vol. XXIV, no. 1, pp. 55–90.

3. Baranov, A.A., Numerical-analytical determination of the parameters of multi-turn rendezvous maneuvers spacecraft in close nearly circular non-coplanar orbits, Space Res., 2008, vol. 46, no. 5, pp. 430–439.

4. D’Amario, L.A., et al., Mars orbit rendezvous strategy for the Mars 2003/2005 sample return mission, AAS/AIAA Astrodynamics Specialist Conference, Girwood, Alaska, August 16–19, 1999, paper AAS 99-306, pp. 1–19.

5. Ocampo, C., Guinn, J., and Breeden, J., Rendezvous options and dynamics for the Mars sample return mission, AAS/AIAA Astrodynamics Specialist Conference, 2001, paper AAS 01-415, pp. 1–20.

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