Rendezvous trajectory design of logistics resupply missions to the lunar gateway in near-rectilinear halo orbit

Author:

Nakamura RyoORCID,Kikuchi Junji,Sasaki TakahiroORCID,Matsumoto Yuki,Hidaka MoekoORCID,Murakami Naomi,Ueda SatoshiORCID,Satoh Naoki

Publisher

Elsevier BV

Subject

Safety, Risk, Reliability and Quality,Aerospace Engineering

Reference15 articles.

1. NASA Technical Reports Server;Lee,2019

2. Practical rendezvous scenario for transportation missions to cis-lunar station in earth-moon L2 halo orbit;Murakami,2015

3. K. Mand, D. Woffinden, P. Spanos, R. Zanetti, “Rendezvous and proximity operations at the earth-moon L2 lagrange point: navigation analysis for preliminary trajectory design,” AAS 14–376.

4. Nonlinear Control Design Techniques for Precision Formation Flying at Lagrange Points;Luquette,2006

5. P.Z. Schulte, P.T. Spehar, D.C. Woffinden, “GN&C sequencing for orion rendezvous, proximity operations, and docking,” 2020 AAS Guidance, Navigation, & Control Conference, AAS 20-045.

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