Nandan Kumar Sinha
Cited by
Cited by
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
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
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
Elementary flight dynamics with an introduction to bifurcation and continuation methods
NK Sinha, N Ananthkrishnan
CRC Press, 2021
A sliding mode controller for aircraft simulated entry into spin
DV Rao, NK Sinha
Aerospace Science and Technology 28 (1), 154-163, 2013
Aircraft spin recovery using a sliding-mode controller
DV Rao, NK Sinha
Journal of guidance, control, and dynamics 33 (5), 1675-1679, 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
Use of the extended bifurcation analysis method for flight control law design
N Sinha, N Ananthkrishnan
40th AIAA Aerospace Sciences Meeting & Exhibit, 249, 2002
Advanced flight dynamics with elements of flight control
NK Sinha, N Ananthkrishnan
CRC Press, 2017
The target guarding problem revisited: Some interesting revelations
RH Venkatesan, NK Sinha
IFAC Proceedings Volumes 47 (3), 1556-1561, 2014
Accessible regions for controlled aircraft maneuvering
AK Khatri, J Singh, NK Sinha
Journal of Guidance, Control, and Dynamics 36 (6), 1829-1834, 2013
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
Aircraft design using constrained bifurcation and continuation method
AK Khatri, J Singh, NK Sinha
Journal of Aircraft 51 (5), 1647-1653, 2014
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
Applications of Bifurcation Methods to F-181HARV Open-loop Dynamics in Landing Configuration
NK Sinha
Defence Science Journal 52 (2), 103, 2002
Nonlinear parameter estimation of airship using modular neural network
S Agrawal, D Gobiha, NK Sinha
The Aeronautical Journal 124 (1273), 409-428, 2020
Direct methodology for constrained system analysis with applications to aircraft dynamics
AS Vora, NK Sinha
Journal of Aircraft 54 (6), 2378-2385, 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
Maximum steady roll rate in zero-sideslip roll maneuvers of aircraft
NK Sinha, N Ananthkrishnan
Journal of aircraft 39 (5), 897-899, 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
The system can't perform the operation now. Try again later.
Articles 1–20