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Halo orbit
The Utilization of Halo Orbit§ in Advanced Lunar Operation§
Astrodynamics
Rendezvous Design in a Cislunar Near Rectilinear Halo Orbit Emmanuel Blazquez, Laurent Beauregard, Stéphanie Lizy-Destrez, Finn Ankersen, Francesco Capolupo
Rideshare and the Orbital Maneuvering Vehicle: the Key to Low-Cost Lagrange-Point Missions
Analysis of Interplanetary Transfers Between the Earth and Mars Halo Orbits
Station-Keeping and Momentum-Management on Halo Orbits Around L2: Linear-Quadratic Feedback and Model Predictive Control Approaches
Utilizing the Deep Space Gateway As a Platform for Deploying Cubesats Into Lunar Orbit
Aas 19-266 Designing Low-Thrust Enabled Trajectories for A
Rendezvous in Cis-Lunar Space Near Rectilinear Halo Orbit: Dynamics and Control Issues
Rendezvous Design in a Cislunar Near Rectilinear Halo Orbit
Long Term Missions at the Sun-Earth Libration Point L1: Ace, Soho, and Wind Aas 11
Generating Exploration Mission-3 Trajectories to a 9:2 Nrho
Periodic Orbit Analytic Construction in the Circular Restricted Three-Body Problem
Low-Thrust Many-Revolution Trajectory Optimization
Optimal Control for Halo Orbit Missions
Ballistic Lunar Transfers to Near Rectilinear Halo Orbit: Operational Considerations
Arxiv:2002.01672V3 [Astro-Ph.EP] 1 Apr 2021
Extended Tisserand-Poincar ´E Graph and Multiple Lunar Swingby Design
Top View
On the Construction of Low-Energy Cislunar and Trans-Lunar Transfers Based on the Libration Points
Easily Retrievable Objects Among the Neo Population
CHARACTERISTICS and DESIGN STRATEGIES for NEAR RECTILINEAR HALO ORBITS WITHIN the EARTH-MOON SYSTEM a Thesis Submitted to the Fa
Aas 17-267 Targeting Cislunar Near Rectilinear Halo
The Pennsylvania State University the Graduate School
Halo Orbit Design and Optimization
When Things Go Wrong: the SOHO Mission Halo Orbit Recovery
Effect of Orbital Shadow at an Earth-Moon Lagrange Point On
Event-Driven Network Model for Space Mission Optimization with High-Thrust and Low-Thrust Spacecraft 1
Low-Energy Transfer to Multi-Circle Elliptic Halo Orbit In
Phasing Orbit Rendezvous”
Development and Optimization of Low Energy Orbits for Advancing Exploration of the Solar System
Optimized Transfers Between Earth-Moon Invariant Manifolds
Supporting a Deep Space Gateway with Free-Return Earth-Moon Periodic Orbits A
Formation Flying Along Halo Orbit Using Switching Hamiltonian Structure-Preserving Control
Orbit Raising Trajectory and System Analysis for the Mission Destiny
Aas 20-488 Motion Primitives Summarizing Periodic Orbits And
Dave Miller Isat Environments Presentation
Analysis of Near Rectilinear Halo Orbit Insertion with a 40-Kw Solar Electric Propulsion System
Spacecraft Propulsion.Pdf
Aas 17-269 Orbit Maintenance and Navigation of Human
Stationkeeping Analysis for Spacecraft in Lunar Near Rectilinear Halo Orbits
IAA-AAS-Dycoss3-125 NEAR RECTILINEAR HALO ORBITS and THEIR APPLICATION in CIS-LUNAR SPACE
An Analytical Theory for the Perturbative Effect of Solar
Low Thrust Transfer to Sun-Earth L1 and L2 Points with a Constraint on the Thrust Direction
Transfer and Rendez-Vous Strategies for the Deployment and the Servicing of an Inhabited Space Station at Earth-Moon L2
Phasing Maneuver Analysis from a Low Lunar Orbit to a Near Rectilinear Halo Orbit
Earth Escape from a Sun-Earth Halo Orbit Using Unstable Manifold and Lunar Swingbys*
Rendezvous Missions to Temporarily-Captured Near Earth Asteroids S Brelsford, Monique Chyba, T Haberkorn, G Patterson
Spacecraft Propulsion, Launch and Orbit Design Rocket Scientists Gift to Exoplanet Scientists
Heliocentric Escape and Lunar Impact from Near Rectilinear Halo Orbits
Low Thrust Trajectory Optimization in Cislunar and Translunar Space by Nathan Luis Olin Parrish B.S., Aerospace Engineering
White Paper: Gateway Destination Orbit Model: a Continuous 15 Year NRHO Reference Trajectory
Transfers to Low Lunar Orbits
AIAA Space 2001 Conference
IAA-AAS-Scitech-039 NEAR RECTILINEAR HALO ORBITS IN
Earth to Halo Orbit Transfer Trajectories
Design and Analysis of Halo Orbits Around L1 Libration Point for Sun-Earth System Pavan M S, Gnanesh C M
Interplanetary Transfer Trajectories Using the Invariant Manifolds of Halo Orbits
Open Mohammad Azhar Thesis.Pdf
A Flexible Lunar Architecture for Exploration (FLARE) Supporting NASA’S Artemis Program