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Vivek Nagabhushan
Vivek Nagabhushan
Millennium Engineering and Integration Company
Verified email at ufl.edu - Homepage
Title
Cited by
Cited by
Year
Attitude control system for small satellites
V Nagabhushan, NG Fitz-Coy, FA Leve
US Patent 9,199,746, 2015
272015
Development of control moment gyroscopes for attitude control of small satellites
V Nagabhushan
University of Florida, 2009
262009
On-orbit jitter control in momentum actuators using a three-flywheel system
V Nagabhushan, NG Fitz-Coy
Acta Astronautica 95, 61-81, 2014
182014
Benefits and challenges of over-actuated excitation systems
N Fitz-Coy, V Nagabhushan, MT Hale
Shock and Vibration 17 (3), 285-303, 2010
142010
Split flywheel assembly with attitude jitter minimization
V Nagabhushan, NG Fitz-Coy
US Patent 8,876,060, 2014
132014
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
122015
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
122015
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
82010
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
62011
Composite and PCB based implementations of a solar panel design for SwampSat
S Asundi, M Mahin, V Nagabhushan, T Yu Lin, N Fitz-Coy
52010
Scalable, HIL, Unconstrained 3-Axis Test Bed for Attitude Control Systems
V Nagabhushan, N Fitz-Coy
AIAA/AAS Astrodynamics Specialist Conference, 8382, 2010
52010
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
52009
Architecture for Unconstrained 3-Axis Attitude Determination and Control Test Bed
V Nagabhushan, S Allgeier, NG Fitz-Coy
Spaceflight Mechanics 140, 2011
42011
PnP attitude control system for responsive space missions
F Leve, V Nagabhushan, N Fitz-Coy
Responsive Space Conference, 2009
42009
Triple flywheel assembly with attitude jitter minimization
NG Fitz-Coy, V Nagabhushan
US Patent 10,005,569, 2018
32018
Rigid rotor balancing using optimization
JS Rao, V Nagabhushan
Advances in Vibration Engineering 9 (1), 25-34, 2010
22010
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
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