Incorporating low-thrust propulsion into the invariant manifolds technique for space trajectories design
Abstract
1.Introduction to non-Keplerianorbits 2.Introduction to the restricted three body problem 3.Introduction to equilibrium points, Halo orbitsand invariant manifolds 4.Dynamical system theory in space trajectory design (transfers to Lagrange point orbits) 5.Introduction of low-thrustpropulsion: controlled RTBP 6.Definition and manipulation of attainable sets 7.End-to-end trajectory optimization: controlled RFBP 8.Results and comparisons (low-thrust, stable-manifoldtransfers to halo orbits) 9.Final remarks
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