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Annika Anderson
Annika Anderson
my.erau.edu üzerinde doğrulanmış e-posta adresine sahip
Başlık
Alıntı yapanlar
Alıntı yapanlar
Yıl
Utilizing the geometric mechanics framework to predict attitude in a full ephemeris model of the Cislunar region
A Anderson, B McCann, D Canales, M Nazari
Communications in Nonlinear Science and Numerical Simulation 130, 107726, 2024
72024
Orbit and Attitude Coupling in the Full Higher-fidelity Ephemeris Model within the Context of the Geometric Mechanics Framework
A Anderson, B McCann, D Canales, M Nazari
AAS/AIAA Spaceflight Mechanics Conference, 2023
62023
Circular restricted full three-body problem with rigid-body spacecraft dynamics in binary asteroid systems
B McCann, A Anderson, M Nazari, D Canales
Celestial Mechanics and Dynamical Astronomy 136 (2), 9, 2024
52024
Resident Space Object Identification in Arbitrary Unresolved Space Images
JD Anderson, AJ Anderson, DA Zuehlke, D Canales, TA Lovell
Proceedings of the 33rd AAS/AIAA Space Flight Mechanics Meeting, 2023
42023
Rigid-Body Spacecraft Dynamics Analysis in a Binary System Using Formulation in Lie Groups
B McCann, A Anderson, M Nazari, D Canales
AAS/AIAA Spaceflight Mechanics Meeting, Austin, TX, 2023
32023
On-Manifold Pose Optimization on SE (3) for Spacecraft Coverage Maximization
BS McCann, A Anderson, M Nazari, D Canales, R Beeson
AAS/AIAA Astrodynamics Specialists Conference, 2023
32023
Benefits of Using a Variational Integrator for the Circular Restricted Full Three-Body Problem
H Gunter, A Anderson, M Nazari, D Canales
AIAA/AAS Astrodynamics Specialist Conference, 2024
12024
Audio Signal Analysis as a Tool in Preventive Maintenance
AJ Anderson
12022
Analysis of LiDAR and Point Cloud Registration Algorithms for Spacecraft Rendezvous and Precision Landing on the Moon
J Schmitt, M Palomo, SG Jo, A Anderson, D Canales Garcia, A Garcia
AIAA SCITECH 2025 Forum, 1415, 2025
2025
GLOBAL ANALYSIS OF OPTIMAL TRAJECTORIES FROM EARTH-MOON 9: 2 NEAR RECTILINEAR HALO ORBIT TO LOW-LUNAR ORBITS
SG Jo, A Sinha, M Palomo, J Graebner, A Anderson, J Schmitt, D Canales, ...
ATTITUDE PREDICTION IN A NEAR-RECTILINEAR HALO ORBIT USING A FULL HIGHER-FIDELITY EPHEMERIS MODEL
A Anderson, H Gunter, D Canales, M Nazari
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