The last 30 years have produced an explosion in the capabilities of designing and managing libration point missions. The starting point was the ground-breaking mission of the third International Sun-Earth Explorer spacecraft (ISEE--3). The ISEE-3 was launched August 12, 1978 to pursue studies of the Earth--Sun interactions, in a first step of what now is known as Space Weather. After a direct transfer of the ISEE-3 to the vicinity of the Sun-Earth Lagrange point, it was inserted into a nearly-periodic halo orbit, in order to monitor the solar wind about 1 h before it reached the Earth's magneto-sphere as well as the ISEE--1 and 2 spacecraft (which where in an elliptical orbit around the Earth).
CITATION STYLE
Belló, M., Gómez, G., & Masdemont, J. J. (2010). Invariant Manifolds, Lagrangian Trajectories and Space Mission Design. In Space Manifold Dynamics (pp. 1–96). Springer New York. https://doi.org/10.1007/978-1-4419-0348-8_1
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