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 | 7 | 2024 |
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 | 6 | 2023 |
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 | 5 | 2024 |
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 | 4 | 2023 |
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 | 3 | 2023 |
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 | 3 | 2023 |
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 | 1 | 2024 |
Audio Signal Analysis as a Tool in Preventive Maintenance AJ Anderson | 1 | 2022 |
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 | | |