9.

Paranjpe, A., Sinha, N.K., and Ananthkrishnan, N., ''Use of Bifurcation and Continuation Methods for Aircraft Trim and Stability Analysis – A State of the Art,'' Journal of Aerospace Sciences and Technologies, Aeronautical Society of India, Vol. 60, No. 2, 2008, pp. 85-100.

00.

Sinha, N.K., and Narang, A., ''A Dynamical System Approach to Compute Pareto Optimal Solution,'' Submitted to Aerospace Science and Technology September 2007, Elsevier Publication, under review.

8.

Sinha, N.K., ''Optimum flight parameters and stability computations using  continuation technique,'' Proceedings of the IMechE Part G, Journal of Aerospace Engineering, Vol. 221, No. 3, 2007, pp. 391-399.

7.

Sinha, N.K., and Hagedorn, P., ''Wind-excited overhead transmission lines: estimation of connection stresses at junctions,'' Journal of Sound and Vibration, Available online November 2006.

6.

Sinha, N.K., and Ananthkrishnan, N., ''Bifurcation Analysis of Inertia-Coupled Roll Maneuvers of Airplanes,'' Journal of Aerospace Engineering, Proc. of IMechE Part G, G04202, Vol. 217, 2003, pp. 75-85.

5.

Sinha, N.K., and Ananthkrishnan, N., ''Maximum Steady Roll-rate in Zero-Sideslip Roll Maneuvers of Aircraft,'' AIAA Journal of Aircraft, Vol. 39, No. 5, 2002, pp. 897-899. 

4.

Sinha, N.K., ''Application of Bifurcation Methods to the F-18/HARV Open-Loop Dynamics in Landing Configuration,'' Defence Science Journal, Vol. 52, No. 2, 2002, pp. 103-115.

3.

Ananthkrishnan, N., and Sinha, N.K., ''Level Flight Trim and Stability Analysis using Extended Bifurcation and Continuation Procedure,'' AIAA Journal of Guidance, Control and Dynamics, Vol. 24, No. 1, 2001, pp. 1225-1228.

2.

Sinha, N.K., ''Application of Bifurcation Methods to Nonlinear Aircraft Dynamics – A Review,'' Journal of the Aeronautical Society of India, Vol. 53, No. 4, 2001, pp. 253-270.

1.

Sudarshan, S., Sinha, N.K., and Ananthkrishnan, N., ''Simplified Spherical Pendulum Model for Rotary Liquid Slosh,'' Journal of the Aeronautical Society of India, Vol. 50, No. 3, 1998, pp. 129-133.

10.

Ananthkrishnan, N., Gupta, N. K., and Sinha, N. K., ''Computational Bifurcation Analysis of Multi-Parameter Dynamical Systems,'' Journal of Guidance, Control, and Dynamics, Vol. 32, No. 5, 2009, pp. 1651-1653.

11.

Rao, D. M. K. V., and Sinha, N.K., ''Aircraft Spin Recovery using a Sliding- Mode Controller,'' Journal of Guidance, Control, and Dynamics, 2010, Accepted for publication.

00.

Narang, A., and Sinha, N.K., ''Feedback Control Law Design Based on Pareto Optimality,'' in preparation.

00.

Rao, D.M.K.V.V., and Sinha, N.K., ''A Sliding Mode Controller for Aircraft Simulated Entry into Spin,'' Aerospace Science and Technology, 2010, revision to be submitted.

00.

Lingala, N., Navin, M., and Sinha, N.K., ''Computing Periodic Orbits and Bifurcations of an Electrodynamic Tethered-Space-System (ETSS) Model using Numerical Continuation,'' in preparation.

18.

Amit K Khatri, and Nandan K Sinha, ''Aircraft Maneuver Design using Bifurcation Analysis and Nonlinear Control Techniques, accepted for presentation in the AIAA ASM Conference, 4-7 Jan 2011, Orlando, FL, USA.

17.

D M K K Venkateswara Rao, Anshu Narang, and Nandan K Sinha, ''Controller Design using Bifurcation Map for Aircraft Spin Recovery, proceedings of the ''WSEAS Dynamical Systems and Control Conference'', 1-3 July 2009, Tenerife, Spain.

16.

D M K K Venkateswara Rao and Nandan K Sinha, ''Bifurcation Map Based Controller Design for Aircraft Spin Entry, proceedings of the ''International Conference and Exhibition on Aerospace Engineering (ICEAE ),'' 18-22 May 2009, IISc, Bangalore, India.

15.

A K Vinayagam, A K Ghosh, and Nandan K Sinha, ''Performance Studies of a Research Aircraft Model using Vectored Thrust, proceedings of the ''International Conference and Exhibition on Aerospace Engineering (ICEAE ),'' 18-22 May 2009, IISc, Bangalore, India.

14.

Lingala, N., Navin, M., and Sinha, N.K., ''Computing Periodic Orbits and Bifurcations of an Electrodynamic Tethered Satellite System (ETSS) Model using Numerical Continuation,'' presented in the 9^th International Conference on Vibration Problems, 19-22 January 2009, IIT Kharagpur, India.

13.

Narang, A., and Sinha, N.K., ''Bifurcation Analysis as a Tool in Advanced Flight Testing,'' International Flight Test Seminar, 14-15 February 2008, ASTE, Bangalore, India.

12.

Paranjpe, A., Sinha, N.K., and Ananthkrishnan, N., ''Use of Bifurcation and Continuation Methods for Aircraft Trim and Stability Analysis – A State-of-the-Art,'' AIAA ASM Conference, Reno, USA, January 8-11, 2007.

11.

Verma, H., Sinha, N.K., and Hagedorn, P., ''Some New Results on the Computation of Wind Power Input for Bundled Conductors via CFD,'' 6^th International Symposium on Cable Dynamics, Charleton, SC, USA, 19-22 September, 2005.

10.

Sinha, N.K., and Hagedorn, P., ''A Mathematical Model for the Computation of Maximum Stress in Long Span Conductor Lines with In-Span Fittings,'' GAMM, Luxembourg, 2005.

9.

Jangid, M., Sinha, N.K., and Ananthkrishnan, N., ''Automated Gain Scheduling using Continuation Technique,'' Nonlinear Control System Conference, IFAC, Sttutgart, Germany, 2004.

8.

Sinha, N.K., Hochlenert, D., Ng., H., and Hagedorn, P., ''Modeling and Analysis of Electrodynamic Tether Dynamics,'' GAMM, Dresden, Germany, 2004.

7.

Kumar, N., Ananthkrishnan, N., and Sinha, N.K., ''Computational Bifurcation Analysis of Multi-Parameter Dynamical Systems,'' NCNSD, IIT Kharagpur, India, December 28-30, 2003.

6.

Sinha, N.K., and Ananthkrishnan, N., ''Automatic Gain Scheduling for Level Flight Stability Augmentation using Continuation Techniques,'' AIAA AFM Conference, Paper # AIAA-2003-5315, TX, USA, 2003.

5.

Sinha, N.K., and Ananthkrishnan, N., ''Dynamical System Analysis of an Aircraft in Landing Approach,'' 24^th National Systems Conference, ISRO, Bangalore, India, December 2002.

4.

Sinha, N.K., and Ananthkrishnan, N., ''Use of the Extended Bifurcation Analysis Method for Flight Control Law Design,'' 40^th AIAA Aerospace Sciences Meeting and Exhibit, Paper # AIAA-2002-0249, Reno, USA, January 2002.

3.

Sinha, N.K., and Ananthkrishnan, N., ''Level Flight Trim and Stability Analysis using Continuation Methods,'' AIAA AFM conference, Paper # AIAA-2000-4112, Denver, USA, August 2000.

2.

Sinha, N.K., and Ananthkrishnan, N., ''Flight Envelope for an Airplane in Roll Maneuvers,'' National Conference on Aerospace and Flight Safety, The Aeronautical Society of India, Goa Branch, May 1999.

1.

Ananthkrishnan, N., and Sinha, N.K., ''Spherical Pendulum as a Possible Model for Rotary Liquid Slosh,'' 48^th AGM of the Aeronautical Society of India, Thiruvananthpuram, India, 1997.