Application of Tisserand's criterion to the design of gravity assist trajectories
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In this paper, a procedure is described for finding these encounter times using Lambert's theorem and a new criterion based on Tisserand's criterion to identify pairs of transfer orbits between the launch planet and intermediate planet and between the intermediate planet and target planet.
[1] Nathan J. Strange,et al. Graphical Method for Gravity-Assist Trajectory Design , 2002 .