| Achieving Climate Change Absolute Accuracy in Orbit BA Wielicki, DF Young, MG Mlynczak, KJ Thome, S Leroy, J Corliss, ... Bulletin of the American Meteorological Society 94 (10), 1519-1539, 2013 | 275 | 2013 |
| Attitude and Orbit Control of a Very Large Geostationary Solar Power Satellite B Wie, CM Roithmayr Journal of Guidance, Control, and Dynamics 28 (3), 439-451, 2005 | 86 | 2005 |
| Contributions of Spherical Harmonics to Magnetic and Gravitational Fields CM Roithmayr | 59 | 2004 |
| Dynamics: Theory and Application of Kane's Method CM Roithmayr, DH Hodges | 58 | 2016 |
| International space station attitude control and energy storage experiment: effects of flywheel torque CM Roithmayr | 37 | 1999 |
| Integrated Orbit, Attitude, and Structural Control System Design for Space Solar Power Satellites B Wie, C Roithmayr | 36 | 2001 |
| Integrated Orbit, Attitude, and Structural Control Systems Design for Space Solar Power Satellites B Wie, C Roithmayr | 36 | 2001 |
| CLARREO approach for reference intercalibration of reflected solar sensors: On-orbit data matching and sampling CM Roithmayr, C Lukashin, PW Speth, G Kopp, K Thome, BA Wielicki, ... IEEE Transactions on Geoscience and Remote Sensing 52 (10), 6762-6774, 2014 | 33 | 2014 |
| Integrated Power and Attitude Control with Spacecraft Flywheels and Control Moment Gyroscopes CM Roithmayr, CD Karlgaard, RR Kumar, DM Bose Journal of Guidance, Control, and Dynamics 27 (5), 859-873, 2004 | 29 | 2004 |
| Fuel-optimal transfers between coplanar circular orbits using variable-specific-impulse engines H Seywald, CM Roithmayr, PA Troutman, SY Park Journal of Guidance, Control, and Dynamics 28 (4), 795-800, 2005 | 20 | 2005 |
| Application of constraint force equation methodology for launch vehicle stage separation BN Pamadi, PV Tartabini, MD Toniolo, CM Roithmayr, CD Karlgaard, ... Journal of Spacecraft and Rockets 50 (1), 191-205, 2013 | 19 | 2013 |
| Modeling multibody stage separation dynamics using constraint force equation methodology PV Tartabini, CM Roithmayr, MD Toniolo, CD Karlgaard, BN Pamadi Journal of Spacecraft and Rockets 48 (4), 573-583, 2011 | 19 | 2011 |
| Fuel-optimal orbital transfers for variable specific impulse powered spacecraft. H Seywald, CM Roithmayr, P Troutman Advances in the Astronautical Sciences 114, 20, 2003 | 17 | 2003 |
| Forces associated with non-linear non-holonomic constraint equations CM Roithmayr, DH Hodges International Journal of Non-Linear Mechanics 45 (4), 357-369, 2010 | 16 | 2010 |
| Verification of a Constraint Force Equation Methodology for Modeling Multi-Body Stage Separation P Tartabini, C Roithmayr, C Karlgaard, M Toniolo, B Pamadi AIAA Modeling and Simulation Technologies Conference and Exhibit, 7039, 2008 | 14 | 2008 |
| Dynamics and control of attitude, power, and momentum for a spacecraft using flywheels and control moment gyroscopes CM Roithmayr, CD Karlgaard, RR Kumar, H Seywald, DM Bose | 13 | 2003 |
| Opportunities to intercalibrate radiometric sensors from International Space Station CM Roithmayr, C Lukashin, PW Speth, DF Young, BA Wielicki, KJ Thome, ... Journal of Atmospheric and Oceanic Technology 31 (4), 890-902, 2014 | 11 | 2014 |
| Relating Constrained Motion to Force Through Newton's Second Law C Roithmayr Georgia Institute of Technology, 2007 | 11 | 2007 |
| Automation of a Versatile Crane (the LSMS) for Lunar Outpost Construction, Maintenance and Inspection W Doggett, C Roithmayr, J Dorsey, T Jones, B King, M Mikulas, H Shen, ... AIAA SPACE 2009 Conference & Exposition, 6546, 2009 | 9 | 2009 |
| International space station attitude motion associated with flywheel energy storage CM Roithmayr AIP Conference Proceedings 504 (1), 454-459, 2000 | 9 | 2000 |
