In this paper, a procedure is described for finding these encounter times using Lambert's theorem and Tisserand's criterion to identify pairs of transfer orbits between the launch planet and intermediate planet and between the intermediate planet and target planet.
Application of Tisserand's criterion to the design of gravity assist trajectories
AIAA Astrodynamics Specialist Conference
2002-08-05
Conference paper
No indication
English
AIAA-2002-4717 Application of Tisserand's Criterion to the Design of Gravity Assist Trajectories
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