Touring Cislunar Periodic Orbit Test Cast for Earth-Moon Search and Rescue

Document Type

Conference Proceeding

Publication Date

1-17-2023

Abstract

This work investigates and analyzes a search and rescue mission comprising a spacecraft in a touring cislunar periodic orbit (TCPO) that will rendezvous with an impaired spacecraft in an near-rectilinear halo orbit (NRHO) about the L2 Lagrange point. This work will simulate a variety of rendezvous' in which both the impaired spacecraft's and the rescuer spacecraft locations are varied. Psuedospectral methods within the circular restricted three-body problem (CR3BP) are utilized to find optimized least time solutions given a max ΔV. The results of this work show the TCPO used in this work to be advantageous in timely rendezvous with an impaired spacecraft in a NRHO.

Source Publication

33rd AAS/AIAA Space Flight Mechanics Meeting

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