Broad-search algorithms for the spacecraft trajectory design of Callisto‐Ganymede‐Io triple flyby sequences from 2024 to 2040, Part II: Lambert pathfinding and trajectory solutions

Broad-search algorithms for the spacecraft trajectory design of Callisto‐Ganymede‐Io triple flyby sequences from 2024 to 2040, Part II: Lambert pathfinding and trajectory solutions

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Article ID: iaor20141126
Volume: 94
Issue: 1
Start Page Number: 253
End Page Number: 261
Publication Date: Jan 2014
Journal: Acta Astronautica
Authors:
Keywords: control
Abstract:

  • Callisto–Ganymede–Io triple flybys can capture a spacecraft into orbit at Jupiter.
  • Lambert solving and V∞ matching found patched-conic solutions for triple flybys.
  • STK was used to find a promising solution that launches from Earth in September 2024.

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