Abstract
The problem of placing and controlling a formation of satellites on a Halo orbit is studied. The Earth-Sun circular restricted three body problem is considered. A family of artificial Halo orbits with the same periods, around the L 1 and L 2 Lagrange points in the Earth-Sun system is found using the pseudo-arc-length continuation method. The orbits are used are reference trajectories for satellites to track. The problem of orbit stability, bounding and controlling the relative motion by means of nonlinear control is addressed.
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Acknowledgements
Claudiu Prioroc’s research has been funded by the European Commission through the Astrodynamics Network AstroNet-II, under Marie Curie contract PITN-GA-2011-289240.
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Prioroc, CL., Mikkola, S. (2016). Low Thrust Relative Motion Control of Satellite Formations in Deep Space. In: Gómez, G., Masdemont, J. (eds) Astrodynamics Network AstroNet-II. Astrophysics and Space Science Proceedings, vol 44. Springer, Cham. https://doi.org/10.1007/978-3-319-23986-6_17
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DOI: https://doi.org/10.1007/978-3-319-23986-6_17
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