| Attitude control system for small satellites V Nagabhushan, NG Fitz-Coy, FA Leve US Patent 9,199,746, 2015 | 28 | 2015 |
| Development of control moment gyroscopes for attitude control of small satellites V Nagabhushan University of Florida, 2009 | 27 | 2009 |
| On-orbit jitter control in momentum actuators using a three-flywheel system V Nagabhushan, NG Fitz-Coy Acta Astronautica 95, 61-81, 2014 | 19 | 2014 |
| Benefits and challenges of over-actuated excitation systems N Fitz-Coy, V Nagabhushan, MT Hale Shock and Vibration 17 (3), 285-303, 2010 | 14 | 2010 |
| Split flywheel assembly with attitude jitter minimization V Nagabhushan, NG Fitz-Coy US Patent 8,876,060, 2014 | 13 | 2014 |
| System and method for assessing the performance of an attitude control system for small satellites NG Fitz-Coy, V Nagabhushan US Patent 9,091,606, 2015 | 12 | 2015 |
| Swampsat-a technology demonstrator for operational responsive space S Allgeier, V Nagabhushan, F Leve, NG Fitz-Coy Proceedings of the 15th CASI (Canadian Aeronautics and Space Institute …, 2010 | 8 | 2010 |
| High fidelity simulation of SwampSat attitude determination and control system JD Munoz, V Nagabhushan, S Asundi, NG Fitz-Coy Spaceflight Mechanics; Univelt, Inc.: San Diego, CA, USA 140, 2011 | 6 | 2011 |
| Composite and PCB based implementations of a solar panel design for SwampSat S Asundi, M Mahin, V Nagabhushan, T Yu Lin, N Fitz-Coy | 5 | 2010 |
| Scalable, HIL, Unconstrained 3-Axis Test Bed for Attitude Control Systems V Nagabhushan, N Fitz-Coy AIAA/AAS Astrodynamics Specialist Conference, 8382, 2010 | 5 | 2010 |
| Split Flywheel Design With Attitude Jitter Minimization Through Flywheel Phase Control V Nagabhushan, N Fitz-Coy AIAA Infotech@ Aerospace Conference and AIAA Unmanned... Unlimited …, 2009 | 5 | 2009 |
| Triple flywheel assembly with attitude jitter minimization NG Fitz-Coy, V Nagabhushan US Patent 10,005,569, 2018 | 4 | 2018 |
| Architecture for Unconstrained 3-Axis Attitude Determination and Control Test Bed V Nagabhushan, S Allgeier, NG Fitz-Coy Spaceflight Mechanics 140, 2011 | 4 | 2011 |
| PnP attitude control system for responsive space missions F Leve, V Nagabhushan, N Fitz-Coy Responsive Space Conference, 2009 | 4 | 2009 |
| Rigid rotor balancing using optimization JS Rao, V Nagabhushan Advances in Vibration Engineering 9 (1), 25-34, 2010 | 2 | 2010 |
| TECHNIQUES FOR IMPROVED PERFORMANCE IN CMG BASED ATTITUDE CONTROL SYSTEMS V Nagabhushan University of Florida, 2013 | | 2013 |
| Estimation of Spacecraft Angular Acceleration using Linear Accelerometers V Nagabhushan, N Fitz-Coy, S Johnson AAS/AIAA Space Flight Mechanics Winter Meeting, 2013 | | 2013 |
| EdUCE, Educate Utilizing CubeSat Experience: a Pragmatic Approach to Shatter Barriers to Space D Buckley, V Shrivante, K Patankar, S Harden, P Muri, N Fitz-Coy | | 2012 |
| On-Orbit Determination of CMG Initial Gimbal Bias Using Sensor Measurements V Nagabhushan, P Barooah, N Fitz-Coy AIAA/AAS Astrodynamics Specialist Conference, 7519, 2010 | | 2010 |
Dr. Frederick A. LeveAir Force Office of Scientific ResearchVerifisert e-postadresse på us.af.mil
