2024/05/29 by Tagliaferri, Flavio, Blazquez, Emmanuel, Acciarini, Giacomo +1
#Chaotic Dynamics (nlin.CD) #FOS: Physical sciences #Space Physics (physics.space-ph)
paper · doi:10.48550/arxiv.2405.18916
This study addresses optimal impulsive trajectory design within the Circular Restricted Three-Body Problem (CR3BP), presenting a global optimization-based approach to identify minimum ΔV transfers between periodic orbits, including heteroclinic connections. By combining a Monotonic Basin Hopping (MBH) algorithm with a sequential quadratic solver in a parallel optimization framework, a wide range of minimum ΔV transfers are efficiently found. To validate this approach, known connections from the literature are reproduced. Consequently, three-dimensional periodic orbits are explored and a systematic search for minimum propellant trajectories is conducted within a selected interval of Jacobi constants and a maximum time of flight. Analysis of the results reveals the presence of very low ΔV solutions and showcases the algorithm's effectiveness across various mission scenarios.