[图书][B] Low-energy lunar trajectory design

JS Parker, RL Anderson - 2014 - books.google.com
Based on years of research conducted at the NASA Jet Propulsion Laboratory, Low-Energy
Lunar Trajectory Design provides high-level information to mission managers and detailed …

Earth–Moon libration point orbit stationkeeping: theory, modeling, and operations

DC Folta, TA Pavlak, AF Haapala, KC Howell… - Acta Astronautica, 2014 - Elsevier
Abstract Collinear Earth–Moon libration points have emerged as locations with immediate
applications. These libration point orbits are inherently unstable and must be maintained …

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 …

The perturbed photogravitational restricted three-body problem: Analysis of resonant periodic orbits

N Pathak, VO Thomas… - Discrete and Continuous …, 2019 - aimsciences.org
In the framework of the perturbed photo–gravitational restricted three–body problem, the first
order exterior resonant orbits and the first, third and fifth order interior resonant periodic …

Representations of higher-dimensional Poincaré maps with applications to spacecraft trajectory design

AF Haapala, KC Howell - Acta Astronautica, 2014 - Elsevier
Abstract The Circular Restricted Three-Body Problem (CR3BP) offers a useful framework for
preliminary trajectory design in multi-body regimes. While the CR3BP offers a simplified …

Incorporating the evolution of multi-body orbits into the trajectory trade space and design process

AF Haapala, KC Howell, DC Folta - Acta Astronautica, 2015 - Elsevier
Libration point orbits have been incorporated in many missions, with the capability of
orbiting near L 1 and L 2 in the Earth–Moon system recently demonstrated during the …

Families of periodic orbits about Lagrangian points L1, L2 and L3 with continuation method

S Yousuf, R Kishor - Planetary and Space Science, 2022 - Elsevier
This study deals the impact of radiation pressure and albedo from the respective primaries in
the context of regularized periodic motion of infinitesimal mass under the frame of restricted …

Баллистико-навигационное обеспечение полётов автоматических космических аппаратов к телам Солнечной системы

ГК Боровин, ЮФ Голубев, АВ Грушевский… - 2018 - elibrary.ru
Книга посвящена ретроспективному обзору прикладных методов современной
небесной механики, использование которых позволило успешно реализовать за более …

Geometry of halo and Lissajous orbits in the circular restricted three-body problem with drag forces

AK Pal, BS Kushvah - Monthly Notices of the Royal Astronomical …, 2015 - academic.oup.com
In this paper, we determine the effect of radiation pressure, Poynting–Robertson drag and
solar wind drag on the Sun–(Earth–Moon) restricted three-body problem. Here, we take the …

Near ballistic halo-to-halo transfers between planetary moons

G Lantoine, RP Russell - The Journal of the Astronautical Sciences, 2011 - Springer
Intermoon transfers are important components of planetary tour missions. However, these
transfers are challenging to design due in part to the chaotic environment created by the …