Design and analysis of a direct transfer trajectory from a near rectilinear halo orbit to a low lunar orbit

Chance-constrained Model Predictive Control for Near Rectilinear Halo Orbit Spacecraft Rendezvous

(2020) Julio C. Sanchez et al.   AEROSPACE SCIENCE AND TECHNOLOGY

Reachable domain of spacecraft with a single normal impulse

(2019) Junhua Zhang et al.   AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY

Transfers from near-rectilinear halo orbits to low-perilune orbits and the Moon’s surface

(2019) Sergey Trofimov et al.   ACTA ASTRONAUTICA

A new method for solving reachable domain of spacecraft with a single impulse

(2018) Qi Chen et al.   ACTA ASTRONAUTICA

Reachable set computation for spacecraft relative motion with energy-limited low-thrust

(2018) Sangjin Lee et al.   AEROSPACE SCIENCE AND TECHNOLOGY

Simple Method to Determine Reachable Domain of Spacecraft with a Single Impulse

(2018) Junhong Duan et al.   JOURNAL OF GUIDANCE CONTROL AND DYNAMICS

Solution Domain Analysis of Earth-Moon Quasi-Symmetric Free-Return Orbits

(2017) BoYong HE et al.   TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

Multibody Orbit Architectures for Lunar South Pole Coverage

(2008) Daniel J. Grebow et al.   JOURNAL OF SPACECRAFT AND ROCKETS