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Survey of station-kee** techniques for libration point orbits
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 …
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 …
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
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 …
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 …
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 …
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
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 …
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
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 …
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 …
give rise to dynamically complex behavior. Thus, design and maintenance of trajectories in …
Orbital guidance using higher-order state transition tensors
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 …
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 …
libration point orbits in series expansions. One of the procedures is based on the Lindstedt …