| 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 | 65 | 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 | 60 | 2007 |
| Elementary flight dynamics with an introduction to bifurcation and continuation methods NK Sinha, N Ananthkrishnan CRC Press, 2021 | 45 | 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 | 44 | 2012 |
| A sliding mode controller for aircraft simulated entry into spin DV Rao, NK Sinha Aerospace Science and Technology 28 (1), 154-163, 2013 | 37 | 2013 |
| Aircraft spin recovery using a sliding-mode controller DV Rao, NK Sinha Journal of guidance, control, and dynamics 33 (5), 1675-1679, 2010 | 36 | 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 | 30 | 2015 |
| Advanced flight dynamics with elements of flight control NK Sinha, N Ananthkrishnan CRC Press, 2017 | 21 | 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 | 20 | 2002 |
| The target guarding problem revisited: Some interesting revelations RH Venkatesan, NK Sinha IFAC Proceedings Volumes 47 (3), 1556-1561, 2014 | 19 | 2014 |
| Accessible regions for controlled aircraft maneuvering AK Khatri, J Singh, NK Sinha Journal of Guidance, Control, and Dynamics 36 (6), 1829-1834, 2013 | 18 | 2013 |
| Applications of Bifurcation Methods to F-181HARV Open-loop Dynamics in Landing Configuration NK Sinha Defence Science Journal 52 (2), 103, 2002 | 16 | 2002 |
| 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 |
| Aircraft design using constrained bifurcation and continuation method AK Khatri, J Singh, NK Sinha Journal of Aircraft 51 (5), 1647-1653, 2014 | 13 | 2014 |
| Nonlinear parameter estimation of airship using modular neural network S Agrawal, D Gobiha, NK Sinha The Aeronautical Journal 124 (1273), 409-428, 2020 | 11 | 2020 |
| 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 |
| Direct methodology for constrained system analysis with applications to aircraft dynamics AS Vora, NK Sinha Journal of Aircraft 54 (6), 2378-2385, 2017 | 10 | 2017 |
| 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 |
| 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 |
| Wind-excited overhead transmission lines: Estimation of connection stresses at junctions NK Sinha, P Hagedorn Journal of sound and vibration 301 (1-2), 400-409, 2007 | 9 | 2007 |
Narayan AnanthkrishnanIndependent ConsultantVerified email at aero.iitb.ac.in
