Level flight trim and stability analysis using extended bifurcation and continuation procedure N Ananthkrishnan, NK Sinha Journal of Guidance, Control, and Dynamics 24 (6), 1225-1228, 2001 | 69 | 2001 |
Use of bifurcation and continuation methods for aircraft trim and stability analysis-a state-of-the-art A Paranjape, N Sinha, N Ananthkrishnan 45th AIAA aerospace sciences meeting and exhibit, 1051, 2007 | 61 | 2007 |
Elementary flight dynamics with an introduction to bifurcation and continuation methods NK Sinha, N Ananthkrishnan CRC Press, 2021 | 50 | 2021 |
Aircraft maneuver design using bifurcation analysis and sliding mode control techniques AK Khatri, J Singh, NK Sinha Journal of Guidance, Control, and Dynamics 35 (5), 1435-1449, 2012 | 49 | 2012 |
A sliding mode controller for aircraft simulated entry into spin DV Rao, NK Sinha Aerospace Science and Technology 28 (1), 154-163, 2013 | 40 | 2013 |
Aircraft spin recovery using a sliding-mode controller DV Rao, NK Sinha Journal of guidance, control, and dynamics 33 (5), 1675-1679, 2010 | 40 | 2010 |
A new guidance law for the defense missile of nonmaneuverable aircraft RH Venkatesan, NK Sinha IEEE Transactions on Control Systems Technology 23 (6), 2424-2431, 2015 | 34 | 2015 |
Advanced flight dynamics with elements of flight control NK Sinha, N Ananthkrishnan CRC Press, 2017 | 26 | 2017 |
Use of the extended bifurcation analysis method for flight control law design N Sinha, N Ananthkrishnan 40th AIAA Aerospace Sciences Meeting & Exhibit, 249, 2002 | 21 | 2002 |
The target guarding problem revisited: Some interesting revelations RH Venkatesan, NK Sinha IFAC Proceedings Volumes 47 (3), 1556-1561, 2014 | 20 | 2014 |
Accessible regions for controlled aircraft maneuvering AK Khatri, J Singh, NK Sinha Journal of Guidance, Control, and Dynamics 36 (6), 1829-1834, 2013 | 19 | 2013 |
Aircraft design using constrained bifurcation and continuation method AK Khatri, J Singh, NK Sinha Journal of Aircraft 51 (5), 1647-1653, 2014 | 14 | 2014 |
An assessment of thrust vector concepts for twin-engine airplane AK Vinayagam, NK Sinha Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2014 | 14 | 2014 |
Nonlinear parameter estimation of airship using modular neural network S Agrawal, D Gobiha, NK Sinha The Aeronautical Journal 124 (1273), 409-428, 2020 | 13 | 2020 |
Direct methodology for constrained system analysis with applications to aircraft dynamics AS Vora, NK Sinha Journal of Aircraft 54 (6), 2378-2385, 2017 | 11 | 2017 |
Configuration analysis of stratospheric airship V Rana, A Kumar, NK Sinha, A Pal, SC Sati Symposium on applied aerodynamics and design of aerospace vehicles, 3-6, 2015 | 11 | 2015 |
Airship trim and stability analysis using bifurcation techniques A Tiwari, A Vora, NK Sinha 2016 7th International Conference on Mechanical and Aerospace Engineering …, 2016 | 10 | 2016 |
Autorotational spin evolving towards chaos MR Wankhede, NK Sinha Journal of aircraft 49 (4), 1183-1188, 2012 | 10 | 2012 |
Bifurcation analysis of inertia coupled roll manoeuvres of airplanes NK Sinha, N Ananthkrishnan Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2003 | 10 | 2003 |
Maximum steady roll rate in zero-sideslip roll maneuvers of aircraft NK Sinha, N Ananthkrishnan Journal of aircraft 39 (5), 897-899, 2002 | 10 | 2002 |