Survey of station-kee** techniques for libration point orbits

M Shirobokov, S Trofimov, M Ovchinnikov - Journal of Guidance …, 2017 - arc.aiaa.org
SINCE the late 1970s, libration points and bounded trajectories around them have become
of practical interest, allowing a number of convenient and useful properties Keplerian motion …

Dynamical systems, the three-body problem and space mission design

WS Koon, MW Lo, JE Marsden… - Equadiff 99: (In 2 Volumes …, 2000 - World Scientific
This paper concerns heteroclinic connections and resonance transitions in the planar
circular restricted 3-body problem, with applications to the dynamics of comets and asteroids …

[КНИГА][B] Dynamics and Mission Design Near Libration Points-Vol I: Fundamentals: The Case of Collinear Libration Points

G Gómez, J Llibre, R Martínez, C Simó - 2001 - books.google.com
In this book the problem of station kee** is studied for orbits near libration points in the
solar system. The main focus is on orbits near halo ones in the (Earth+ Moon)-Sun system …

[PDF][PDF] Stationkee** analysis for spacecraft in lunar near rectilinear halo orbits

D Guzzetti, EM Zimovan… - 27th AAS/AIAA …, 2017 - engineering.purdue.edu
Near Rectilinear Halo Orbits (NRHOs), a subset of the halo orbits characterized by favorable
stability properties, are strong candidates for a future inhabited facility in the lunar vicinity. To …

A review of periodic orbits in the circular restricted three-body problem

R Zhang - Journal of Systems Engineering and Electronics, 2022 - ieeexplore.ieee.org
This review article aims to give a comprehensive review of periodic orbits in the circular
restricted three-body problem (CRTBP), which is a standard ideal model for the Earth-Moon …

Study of the transfer from the Earth to a halo orbit around the equilibrium pointL 1

G Gómez, A Jorba, J Masdemont, C Simó - Celestial Mechanics and …, 1993 - Springer
The purpose of this paper is to study a transfer strategy from the vicinity of the Earth to a halo
orbit around the equilibrium point L 1 of the Earth-Sun system. The study is done in the real …

[PDF][PDF] Station-kee** strategies for translunar libration point orbits

G Gómez, KC Howell, J Masdemont… - Advances in …, 1998 - researchgate.net
Spacecraft in orbits near the collinear libration points are proving to be excellent platforms
for scientific investigations of various phenomena. Since such libration point trajectories are …

Trajectory design and orbit maintenance strategies in multi-body dynamical regimes

TA Pavlak - 2013 - search.proquest.com
Regions of space in which multiple, simultaneous gravitational influences are present often
give rise to dynamically complex behavior. Thus, design and maintenance of trajectories in …

Orbital guidance using higher-order state transition tensors

S Boone, J McMahon - Journal of Guidance, Control, and Dynamics, 2021 - arc.aiaa.org
This paper derives the equations necessary to use state transition tensors (STTs) in a
spacecraft guidance problem. The derivation includes all necessary equations up to the …

High-order expansions of invariant manifolds of libration point orbits with applications to mission design

JJ Masdemont* - Dynamical Systems, 2005 - Taylor & Francis
This paper deals with two methodologies for computing the stable and unstable manifolds of
libration point orbits in series expansions. One of the procedures is based on the Lindstedt …