| ORION: A simulation environment for spacecraft formation flight, capture, and orbital robotics M Wilde, B Kaplinger, T Go, H Gutierrez, D Kirk 2016 IEEE Aerospace Conference, 1-14, 2016 | 54 | 2016 |
| Conceptual design of a hypervelocity asteroid intercept vehicle (HAIV) and its flight validation mission A Pitz, B Kaplinger, G Vardaxis, T Winkler, B Wie Acta Astronautica 94 (1), 42-56, 2014 | 45 | 2014 |
| Nuclear fragmentation/dispersion modeling and simulation of hazardous near-Earth objects B Kaplinger, B Wie, D Dearborn Acta Astronautica 90 (1), 156-164, 2013 | 27 | 2013 |
| GPU-based optical navigation and guidance for a hypervelocity asteroid intercept vehicle (HAIV) JR Lyzhoft, BD Kaplinger, B Wie, MJ Hawkins AIAA Guidance, Navigation, and Control (GNC) Conference, 4966, 2013 | 25 | 2013 |
| GPU accelerated 3D modeling and simulation of a blended kinetic impact and nuclear subsurface explosion BD Kaplinger, C Setzer, B Wie AIAA Guidance, Navigation, and Control (GNC) Conference, 4548, 2013 | 19 | 2013 |
| Earth-impact modeling and analysis of a near-Earth object fragmented and dispersed by nuclear subsurface explosions B Kaplinger, B Wie, D Dearborn The Journal of the Astronautical Sciences 59, 101-119, 2012 | 18 | 2012 |
| Preliminary results for high-fidelity modeling and simulation of orbital dispersion of asteroids disrupted by nuclear explosives B Kaplinger, B Wie, D Dearborn AIAA/AAS Astrodynamics Specialist Conference, 7982, 2010 | 15 | 2010 |
| Computational solutions to Lambert’s problem on modern graphics processing units S Wagner, B Wie, B Kaplinger Journal of Guidance, Control, and Dynamics 38 (7), 1305-1311, 2015 | 14 | 2015 |
| An Innovative Solution to NASA's NEO Impact Threat Mitigation Grand Challenge and Flight Validation Mission Architecture Development B Wie, B Barbee, A Pitz, B Kaplinger, M Hawkins, T Winkler, P Premaratne, ... | 14 | 2014 |
| Optical navigation and fuel-efficient orbit control around an irregular-shaped asteroid T Winkler, BD Kaplinger, B Wie AIAA Guidance, Navigation, and Control (GNC) Conference, 5117, 2013 | 14 | 2013 |
| GPU accelerated genetic algorithm for multiple gravity-assist and impulsive V maneuvers S Wagner, B Kaplinger, B Wie AIAA/AAS Astrodynamics Specialist Conference, 4592, 2012 | 12 | 2012 |
| ORION: a teaching and research platform for simulation of space proximity operations M Wilde, BD Kaplinger, TH Go AIAA SPACE 2015 conference and exposition, 4427, 2015 | 11 | 2015 |
| A preliminary study on nuclear standoff explosions for deflecting near-Earth objects B Kaplinger, B Wie, J Basart Proceedings of the 1st IAA Planetary Defense Conference, 27-30, 2009 | 10 | 2009 |
| Efficient Parallelization of Nonlinear Perturbation Algorithms for Orbit Prediction with Applications to Asteroid Deflection BD Kaplinger, B Wie, D Dearborn presented as paper AAS, 10-225, 2010 | 7 | 2010 |
| Comparison of Fragmentation/Dispersion Models for Asteroid Nuclear Disruption Mission Design B Kaplinger, B Wie presented as paper AAS, 11-403, 2011 | 6 | 2011 |
| Optimized GPU simulation of a disrupted near-Earth object including self-gravity B Kaplinger, B Wie presented as paper AAS-11-266 at the 21st AAS/AIAA Space Flight Mechanics …, 2011 | 6 | 2011 |
| Establishment and design of an earth-moon communications network in lunar polar orbit A Genova, B Kaplinger, M Wilde, B Aldrin 2018 IEEE Aerospace Conference, 1-9, 2018 | 5 | 2018 |
| Conceptual Design of a Hypervelocity Asteroid Intercept G Vardaxis, T Winkler, B Wie, A Pitz, B Kaplinger Asteroid Deflection Research Center, Iowa State University. USA: IA, 50011-2271, 2012 | 5 | 2012 |
| Preliminary design of a hypervelocity nuclear interceptor system (HNIS) for optimal disruption of near-earth objects A Pitz, B Kaplinger, B Wie, D Dearborn 22nd Spaceflight mechanics 2012, 29 January-2 February 2012, 2012 | 5 | 2012 |
| Parameter variation in near-Earth object disruption simulations using GPU acceleration B Kaplinger, B Wie presented as paper AAS-11-267 at the 21st AAS/AIAA Space Flight Mechanics …, 2011 | 5 | 2011 |
