| Mars conjunction crewed missions with a reusable hybrid architecture RG Merrill, N Strange, M Qu, N Hatten 2015 IEEE Aerospace Conference, 1-14, 2015 | 33 | 2015 |
| A smooth and robust Harris-Priester atmospheric density model for low Earth orbit applications N Hatten, RP Russell Advances in Space Research 59 (2), 571-586, 2017 | 15 | 2017 |
| A critical evaluation of modern low-thrust, feedback-driven spacecraft control laws NA Hatten | 14 | 2012 |
| Parallel implicit Runge-Kutta methods applied to coupled orbit/attitude propagation N Hatten, RP Russell The Journal of the Astronautical Sciences 64 (4), 333-360, 2017 | 13 | 2017 |
| Applications of Machine Learning and Monocular Vision for Autonomous On-Orbit Proximity Operations N Dhamani, G Martin, C Schubert, P Singh, N Hatten, MR Akella AIAA Scitech 2020 Forum, 1376, 2020 | 12 | 2020 |
| Comparison of three Stark problem solution techniques for the bounded case N Hatten, RP Russell Celestial Mechanics and Dynamical Astronomy 121 (1), 39-60, 2015 | 9 | 2015 |
| OSIRIS-REx Extended Mission Trajectory Design & Target Search B Sutter, N Hatten, KM Getzandanner, KM Hughes, D Wibben, K Williams, ... AIAA SCITECH 2022 Forum, 2469, 2022 | 8 | 2022 |
| OSIRIS-APEX: An OSIRIS-REx Extended Mission to Asteroid Apophis DN DellaGiustina, MC Nolan, AT Polit, MC Moreau, DR Golish, AA Simon, ... The Planetary Science Journal 4 (10), 198, 2023 | 6 | 2023 |
| The eccentric case of a fast-rotating, gravity-gradient-perturbed satellite attitude solution N Hatten, RP Russell Celestial Mechanics and Dynamical Astronomy 130 (11), 71, 2018 | 6 | 2018 |
| Terrain Relative Navigation in a Lunar Landing Scenario Using autoNGC MA Shoemaker, S Hur-Diaz, A Liounis, J Van Eepoel, M Romeo, V Wu, ... AIAA SciTech 2022 Forum, 0744, 2022 | 5 | 2022 |
| Decoupled Direct State Transition Matrix Calculation with Runge-Kutta Methods N Hatten, RP Russell The Journal of the Astronautical Sciences 65 (3), 321-354, 2018 | 5 | 2018 |
| Semianalytical Technique for Six-Degree-of-Freedom Space Object Propagation N Hatten, RP Russell Journal of Guidance, Control, and Dynamics 42 (2), 217-228, 2019 | 4 | 2019 |
| Ground-based Tracking of Geosynchronous Space Objects with a GM-CPHD Filter BA Jones, N Hatten, N Ravago, RP Russell Advanced Maui Optical and Space Surveillance Technologies (AMOS), 2016 | 4 | 2016 |
| Fast Earth-Mars Roundtrip Trajectories to Reduce Health and Safety Risks for Crewed Missions N Hatten, K Hughes, DC Folta, A Valinia 2022 AAS/AIAA Astrodynamics Specialist Conference, 2022 | 3 | 2022 |
| Trajectory Optimization for OSIRIS-REx Earth Return N Hatten, JA Englander, DH Ellison, R Nakamura, B Sutter, KE Williams, ... AAS/AIAA Astrodynamics Specialist Conference, 2020, 4703-4720, 2021 | 2 | 2021 |
| Determination and Realization of Arrival and Departure Orbits for Mars Exploration N Hatten, RG Merrill NASA Systems Analysis and Concepts Directorate, 2013 | 2 | 2013 |
| Space object translational and rotational state prediction and sensitivity calculation NA Hatten | 1 | 2016 |
| APPLICATION OF THE STARK PROBLEM TO SPACE TRAJECTORIES WITH TIME-VARYING PERTURBATIONS N Hatten, RP Russell methods 6, 12, 0 | 1 | |
| An Infeasible Interior-Point Arc-Search Algorithm for Spacecraft Trajectory Optimization Y Yang, R Pritchett, N Hatten 2024 INFORMS Optimization Society Conference, 2024 | | 2024 |
| Risk trade-space analysis for safe human expeditions to Mars A Valinia, D Folta, K Hughes, N Hatten, A Vera, L Stone, M Parisi, ... Acta Astronautica 211, 192-199, 2023 | | 2023 |
Ryan P. RussellProfessor, Aerospace Engineering, University of Texas at AustinVerified email at austin.utexas.edu
