Low Thrust Relative Motion Control of Satellite Formations in Deep Space




Prioroc CL, Mikkola S

Gerard Gómez, Josep J. Masdemont

Astrodynamics Network AstroNet-II

PublisherSPRINGER INT PUBLISHING AG, GEWERBESTRASSE 11, CHAM, CH-6330, SWITZERLAND

2016

Astrodynamics Network AstroNet-II: The Final Conference

ASTRODYNAMICS NETWORK ASTRONET-II: THE FINAL CONFERENCE

ASTROPHYSICS SPACE

Astrophysics and Space Science Proceedings

44

241

256

16

978-3-319-23984-2

978-3-319-23986-6

1570-6591

DOIhttps://doi.org/10.1007/978-3-319-23986-6_17



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.



Last updated on 2024-26-11 at 22:05