| Modeling and numerical simulation of linear and nonlinear spacecraft attitude dynamics and gravity gradient moments: A comparative study MD M. Navabi, N. Nasiri Communications in Nonlinear Science and Numerical Simulation 17 (2), 1065–1084, 2012 | 35 | 2012 |
| Simulating the Earth Magnetic Field According to the 10th Generation of IGRF Coefficients for Spacecraft Attitude Control Applications NN M. Navabi 5th International Conference on Recent Advances in Space Technologies 3, 584-588, 2011 | 17 | 2011 |
| Orbital and attitude control of a spacecraft around an asteroid M Reyhanoglu, NN Kamran, K Takahiro 2012 12th International Conference on Control, Automation and Systems, 1627-1632, 2012 | 15 | 2012 |
| Observer Design for Distributed Parameter Systems NN Kamran, SV Drakunov SIAM Conference on Control and its Applications, 2015 | 7 | 2015 |
| Sliding Mode Observers for Distributed Parameter Systems: Theory and Applications NN Kamran | 3 | 2016 |
| Sliding mode observer for fluid flow NN Kamran, SV Drakunov 2017 IEEE Conference on Control Technology and Applications (CCTA), 1195-1200, 2017 | 2 | 2017 |
| Nonlinear observer for distributed parameter systems described by decoupled advection equations NN Kamran, SV Drakunov, WM Solano Journal of Vibration and Control, 1-14, 2015 | 2 | 2015 |
| Electrical Energy Optimization in Spacecraft Attitude Control System Using Proper Configuration of Actuators NN M. Navabi 24th European Conference on Operational Research, 2010 | | 2010 |
| Three-Axis Stabilization of a Low Earth Orbit pacecraft Utilizing Three Magnetorquers and Reaction Wheels Combinations, According to Energy Consumption NN M. Navabi 61st International Astronautical Congress, 2010 | | 2010 |
Sergey V DrakunovProfessor, Embry-Riddle Aeronautical University, FloridaVerified email at erau.edu
