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Publications

Referred Journals

  1. Lee, K. W., and Singh, S. N., "Composite Adaptive Control and Identification of MIMO Aeroelastic System with Enhanced Parameter Excitation," ASCE Journal of Aerospace Engineering, 35(6), 2022, pp. 04022093-1 - 04022093-17, DOI: 10.1061/(ASCE)AS.1943-5525.0001490.
  2. Lee, K. W., and Singh, S. N., "Composite Adaptive Attitude Control of Asteroid-Orbiting Spacecraft with Regressor Integral Excitation," IEEE Trans. on Aerospace and Electronic Systems, March 2022. (8 pages).DOI: 10.1109/TAES.2022.3164011.
  3. Lee, K. W., and Singh, S. N., "Passivity-based adaptive control of aeroelastic system with unsteady aerodynamics and wind gust,"Mathematics in Engineering, Science, and Aerospace (MESA)," Vol. 12, No. 4, November 2021, pp. 1103-1117. [Cambridge : Cambridge Scientific Publishers. (print) ISSN 2041-31734Cambridge, UK.
  4. Lee, K. W. and Singh, S. N., "Immersion and Invariance Based Adaptive Attitude Control ofAsteroid-Orbiting Spacecraft Using Modified Rodrigues Parameters," Aeronautics & Aerospace Open Access Journal, Vol. 5, Issue 2, pp. 57-64, July 2021 eISSN: 2576-4500, DOI: 10.15406/aaoaj.2021.05.00128 (Publisher MedCrave)
  5. Lee, K. W. and Singh, S. N, "Generalized composite noncertainty-equivalence adaptive control of a prototypical wing section with torsional nonlinearity," Nonlinear Dynamics, Vol. 103, Feb. 2021 pp. 2547-2561, Springer, .DOIhttps://doi.org/10.1007/s11071-021-06227-3
  6. Lee, K. W. and Singh, S. N, "Generalized Composite Noncertainty-EquivalenceAdaptive Control of Orbiting Spacecraft in Vicinityof Asteroid,"The Journal of the Astronautical Sciences, Vol. 67, Issue 3, Sept. 2020, pp. 1021- 1043, https://doi.org/10.1007/s40295-019-00207-x
  7. Lee, K. W. and Singh, S. N, "Quaternion-based adaptive attitude control of asteroid-orbiting spacecraftvia immersion and invariance," Acta Astronautica, Volume 167, February 2020, Pages 164-180, https://doi.org/10.1016/j.actaastro.2019.10.031.
  8. Lee, K. W. and Singh, S. N, "Noncertainty-equivalence adaptive attitudecontrol of satellite orbiting around anasteroid," Acta Astronautica, May 5, 2019. doi.org/10.1016/j.actaastro.2019.05.008.
  9. Lee, K. W. and Singh, S. N, "Immersion-and Invariance-based Adaptive Control of Asteroid-Orbiting and-Hovering Spacecraft,"Journal of Astronaurtical Sciences, April 2019.
  10. Lee, K. W. and Singh, S. N., "Adaptive and Super-Twisting Adaptive Spacecraft Orbit Control Around Asteroids," ASCE Journal of Aerospace Engineering, 32(4): 04019042 (14 pages), 2019 DOI: 10.1061/(ASCE)AS.1943-5525.0001043.
  11. Lee, K. W. and Singh, S. N, "Robust Finite-Time Continuous Control of an Unsteady Aeroelastic System," AIAA Journal of Guidance, Control and Dynamics,Vol. 41, No. 4 (2018), pp. 978-986. doi.org/10.2514/1.G003087
  12. Raj, K., Muthukumar, V., Singh, S. N., and Lee, K.W., "Finite-time sliding mode and super-twisting control of fighter aircraft," Aerospace Science and Technology, Vol. 82-83, November 2018, Pages 487-498. (accepted Sept 24, 2018)
  13. Lee, K. W. and Singh, S. N., "L1 Adaptive Control of an Aeroelastic System with Unsteady Aerodynamics and Gust Load, "Journal of Vibration and Control, Vol. 24, No. 2, pp. 303- 322, 2018.
  14. Lee, K. W. and Singh, S. N, "Longitudinal Nonlinear Adaptive Autopilot Design for Missiles with Control Constraint," Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Vol. 232(9), pp. 1655-1670, 2018. doi.org/10.1177/0954410017699002
  15. Lee, K. W. and Singh, S. N, "Noncertainty-Equivalence Spacecraft Adaptive Formation Control with Filtered Signals," ASCE Journal of Aerospace Engineering J. Aerosp. Eng., 2017, 30(5): 04017029 (12 pages).
  16. Lee, K. W. and Singh, S. N., "Immersion and Invariance-Based Adaptive Wing Rock Control with Nonlinear Terminal Manifold, "Nonlinear Dynamics, Vol. 88, Issue 2, April, 2017, pp. 955-972 .DOI :10.1007/s11071-016-3287-y.
  17. Lee, K. W., Ghorawat, P., and Singh, S. N., "Wing Rock Control by Finite Form Adaptation," Journal of Vibration and Control, Vol. 22, No. 11, June 2016, pp. 2687-2703.
  18. Lee, K. W. and Singh, S. N., "Nonlinear Adaptive trajectory control of MIMO submarineswith input constraints," Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering, Vol. 230, No. 2, 2016,pp. 164-183.
  19. Lee, K. W. and Singh, S. N., "A Higher-order Sliding Mode Three-Axis Solar Pressure Satellite Attitude Control System," Journalof Aerospace Engineering, Vol. 29, Issue 1, January 2016, (15 pages), DOI: 10.1061/(ASCE)AS.1943-5525.0000509.
  20. Lee, K. W. and Singh, S. N., "Adaptive Control of Multi-Input Aeroelastic System with Constrained Inputs," AIAA Journal of Guidance, Control and Dynamics, Vol. 38, Issue 12, December 2015, pp. 2337-2350. doi: 10.2514/1.G001022
  21. Lee, K. W. and Singh, S. N."Three-Axis L1 Adaptive Attitude Control of Spacecraft Using Solar Radiation Pressure," Proceedings of the Institution of MechanicalEngineers Part G: Journal of Aerospace Engineering, Vol. 229(3), 2015, pp. 407-422 doi: 10.1177/0954410014533943.
  22. Chalike, S. K., Lee, K. W. and Singh, S. N."Synchronization of Inferior Olive Neurons Via L1 Adaptive Feedback," Nonlinear Dynamics, Vol. 78, Issue 1, October 2014, pp. 467-483. (DOI) 10.1007/s11071-014-1454-6.
  23. Lee, K. W. and Singh, S. N., "Robust Higher-Order Sliding Mode Finite-Time Control of Aeroelastic Systems," AIAA Journal of Guidance, Control and Dynamics, Vol. 37, No. 5, September/October 2014, pp. 1664-1670, DOI: 10.2514/1.G000456.
  24. Lee, K. W. and Singh, S. N., "L1 Adaptive Control of Projectile Fin by Piezoelectric Actuator, "Journalof Aerospace Engineering, Volume 27, Issue 4 (July 2014), 10.1061/(ASCE)AS.1943-5525.0000288 , 06014002.
  25. Lee, K. W. and Singh, S. N., "Multi-Input Submarine Control Via L1 Adaptive Feedback Despite Uncertainties," Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering, Vol. 228 (5), 2014, pp. 330-347, doi:10.1177/0959651813515206.
  26. Lee, K. W. and Singh, S. N., "Noncertainty-Equivalent Adaptive Wing Rock Control Via Chebyshev Neural Network," AIAA Journal of Guidance, Control and Dynamics, Vol. 37, No. 1, Jan-Feb 2014, pp. 123-133.
  27. Lee, K. W. and Singh, S. N., "L_1 Adaptive Attitude Control of Satellites in Elliptic Orbits Using Solar RadiationPressure" Proceedings of the Institution of MechanicalEngineers Part G: Journal of Aerospace Engineering, Vol. 228, No. 4, March 20, 2014, pp. 611-626, DOI: 0954410013478510.
  28. Maganti, G. B., Singh, S. N., and Yim, W., "Control of a Magnetorheological Fluid Vibration Damping System Via Feedback Linearization and Suboptimal Design," Journal of Control Engineering and Technology, Vol. 3, Issue 4, 2013, pp. 166-174.
  29. Lee, K. W. and Singh, S. N., "$ L_1$ Adaptive Control of aNonlinear Aeroelastic System Despite Gust Load," Journal of Vibration and Control, Vol. 19, No. 12, September 2013, pp. 1807-1821.
  30. Lee, K. W. and Singh, S. N., "Noncertainty-Equivalent Multi-variable Adaptive Control of Submersibles Using Filtered Signals," Ocean Engineering, Vol. 53, October 2012, pp. 98-110.
  31. Lee, K. W. and Singh, S. N., "L_1 Adaptive Control of Flexible Spacecraft Despite Disturbances," Acta Astronautica, Vol. 80, November- December 2012, pp. 24-35.
  32. Lee, K. W. and Singh, S. N., "Bifurcation of Orbits and Synchrony in Inferior Olive Neurons," Journal of Mathematical Biology, Vol. 65, No. 3, September 2012, pp. 465-491.
  33. Lee, K. W. and Singh, S.N., "Immersion- and Invariance-Based Adaptive Missile ControlUsing Filtered Signals," Proceedings of the Institution of MechanicalEngineers Part G: Journal of Aerospace Engineering, Vol. 226, Issue 6, June 2012, pp. 646-663.
  34. Lee, K. W. and Singh, S. N., "Variable Structure Model Reference Adaptive Formation Control of Spacecraft," AIAA Journal of Guidance, Control and Dynamics, Vol 35, No. 1, January-February 2012,pp. 104-115.
  35. Lee, K. W. and Singh, S.N., "Tuning Functions-Based Output Feedback Adaptive Spacecraft Formation FlyingDespite Disturbances," Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering,Vol. 226, No. 1, January 2012, pp. 15-29.
  36. Lee, K. W. and Singh, S.N., "Non-Certainty-Equivalent Adaptive Controlof Chaos in Lorenz System," International Journal of Modeling, Identification andControl, Vol. 13, No. 4, 2011, pp. 310-318.
  37. Lee, K. W. and Singh, S.N., "Non-Certainty-Equivalent Adaptive Control ofa Nonlinear Aeroelastic System,"International Journal of Electronics and Telecommunications,Vol. 56, No. 4, 2010, pp. 463-471.
  38. Lee, K. W. and Singh, S. N., "Attractive Manifold-Based Adaptive Solar AttitudeControl of Satellites in Elliptic Orbits," Acta Astronautica,Vol. 68, No. 1-2, January-February 2011, pp. 185-196.
  39. Lee, K. W. and Singh, S. N., "Multi-Input Noncertainty-Equivalent AdaptiveControl of an Aeroelastic System," AIAA Journal of Guidance, Control and Dynamics, Vol. 33, No. 5, September-October 2010,pp. 1451-1460.
  40. Lee, K. W. and Singh, S. N., "Noncertainty-Equivalent AdaptiveMissile Control Via Immersion and Invariance," AIAA Journal of Guidance, Control and Dynamics, Vol. 33, No. 3, May-June 2010,pp. 655-665.
  41. Ramasamy, S. and Singh, S. N., "Biology-Inspired Robust Dive Plane Control of Nonlinear AUV using Pectoral-Like Fins,"Applied Bionics and Biomechanics, Vol. 7, No. 2, June 2010, pp. 153-168.
  42. Gutta, S. and Singh, S. N., "Output Feedback Control of Smart Projectile Fin Based on Internal Model Principle," 2009 ASME Early Career Technical Journal, 2009, p. 9.1-9.8.
  43. Lee, K. W. and Singh, S. N., "Adaptive Global Synchrony of InferiorOlive Neurons," Bioinspiration and Biomimetics, 4 036003, 2009.
  44. Lee, K. W. and Singh, S.N., "Noncertainty-Equivalent Adaptive SatelliteAttitude Control Using Solar Radiation Pressure, Proceedings ofInstitute of Mechanical Engineers, Part G, Journal of Aerospace Engineering,Vol 223(G7), 977-988, Nov. 2009.
  45. Lee, K. W. and Singh, S.N., "Immersion and Invariance Based Adaptive Control ofa Nonlinear Aeroelastic System," AIAA Journal of Guidance, Control, and Dynamics,Vol. 32, No. 4, pp. 1100-1110,July-August 2009.
  46. Nambisan, P., and Singh, S.N., "Adaptive Output FeedbackControl of MIMO AUV With Unknown Gain Matrix,"Systems Science, Vol. 35, No. 2, 2009, pp. 5-10.
  47. Naik, M, Singh, S. N., and Mittal, R., "Indirect Adaptive Output Feedback Control of a biorobotic AUV Using Pectoral-like Mechanical Fins," Bioinspiration and Biomimetics, Vol 4, No. 2, ( 11 pages), June 2009.
  48. Nambisan, P., and Singh, S.N., "Multi-variableAdaptive Backstepping Control of Submersibles Using SDU Decomposition," Ocean Engineering, Volume 36, Issue 2, pp. 133-212, February 2009.
  49. Bandyopadhyay, P.R., Singh, S.N., Thivierge, D.P., Annaswamy, A.M., Leinhos, H.A., Fredette, A.R., and Beal, D.N., "Synchronization of Animal-InspiredMultiple High-Lift Fins in an Underwater Vehicle Using Olivo-Cerebellar Dynamics," IEEE Journal of Oceanic Engineering, Vol. 33 (4), pp. 563-578, 2008.
  50. Lee, K.W., Nambisan, P., and Singh, S.N., "Adaptive and Variable Structure Control ofAircraft with Unknown High-Frequency Gain,"Journal of Guidance, Control, and Dynamics, Vol. 31, No. 1, Jan. 2008, pp.194-203.
  51. Naik, M., and Singh, S. N., "Oscillatory Adaptive Yaw Plane Controlof Biorobotic AUV Using Pectoral-Like Fins," Applied Bionics and Biomechanics,Vol. 4, No. 4, 2007, pp. 137-147.
  52. Nambisan, P., and Singh, S.N, "Nonlinear Robust Output Feedback Controlof Submersibles Via Modeling Error Compensation," Systems Science,Vol. 33, No. 4, 2007, pp. 27-35.
  53. Maganti, G. B. and Singh, S.N., "Simplified Adaptive Control of an Orbiting Spacecraft," Acta Astronautica, Vol. 61, Issues-6-7, 2007, pp. 578-589.
  54. Naik, M.S. and Singh, S.N., "State-Dependent Riccati Equation-Based RobustDive Plane Control of AUV with Control Constraints," Ocean Engineering,Vol. 34, 2007, pp. 1711-1723.
  55. Mani, S., Singh, S.N., Parimi, S. K., and Yim, W., "AdaptiveServoregulation of a Projectile Fin Using Piezoelectric Actuator,"ASME Transactions Journal of Dynamic Systems, Measurement, andControl, Vol. 129, No. 1, January 2007, pp. 100-104.
  56. Lee, K. W., and Singh, S.N., "Robust Control of Chaos in Chua'sCircuit Based on Internal Model Principle," Chaos, Solitons, & Fractals,Issue 5, March 2007, pp. 1095-1107..
  57. Lee, K. W. and Singh, S.N., "Global Robust Control of an Aeroelastic System Using Output Feedback, "Journal of Guidance, Control, andDynamics, Vol. 30, No. 1, January-February 2007, pp. 271-275.
  58. Narasimhan, M., Dong, H., Mittal, R., and Singh, S.N., "OptimalYaw Regulation and Trajectory Control of Biorobotic AUV Using Mechanical Fins Based on CFD Parameterization," ASME Transactions Journalof Fluids Engineering, Vol. 128, July 2006, pp. 687-698.
  59. Narasimhan, M., and Singh, S. N., "Adaptive Input-Output FeedbackLinearizing Yaw Plane Control of BAUV Using Dorsal Fins," Ocean Engineering, Vol. 33, Issues 11-12, August 2006, pp. 1413-1430.
  60. Maganti, G., and Singh, S. N., "Output Feedback Form of Chua'sCircuit and Modular Adaptive Control ofChaos Using Single Measurement," Chaos, Soliton and Fractals, Vol. 28,No. 3, 2006,pp. 724-738.
  61. Narasimhan, M., and Singh, S. N., "Adaptive Optimal Control of an AutonomousUnderwater Vehicle in Dive plane Using Dorsal Fins," Ocean Engineering,Vol. 33, April 2006, pp. 404-416.
  62. Singh, S.N., and Mani, S., "Control of Oscillating Foil for Propulsion of Biorobotic AUV," Applied Bionics & Biomechanics, Vol. 2, Issue 2, 2005,pp. 117-123.
  63. Mani, S., Singh, S.N., Parimi, S. K., Yim, W., and Trabia, M., "Adaptive Rotation of a Smart Projectile Fin by Piezoelectric Flexible Beam Actuator," Journal of Vibration and Control, Vol. 11, No. 8, August 2005,pp. 1085-1102.
  64. Maganti, G., and Singh, S. N., "Modular Adaptive Control ofChaos in Chua'sCircuit," International Journal of Bifurcation and Chaos, Vol. 15, No. 9, 2005,pp. 2973-2984.
  65. Singh, S. N., and Yim, W., "Nonlinear AdaptiveSpacecraft AttitudeControl Using Solar Radiation Pressure," IEEE Transaction on Aerospace and Electronic Systems,Vol. 41, No. 3, July 2005, pp. 770-779.
  66. Gujjula, S., and Singh, S. N., "Variable Structure Control of Unsteady Aeroelastic System with Partial State Information," AIAA Journal of Guidance,Control, and Dynamics, Vol. 28, No. 1, May-June 2005, pp. 568-573.
  67. Gujjula, S., Singh, S. N., Yim, W., "Adaptive and Neural Controlof a Wing Section Using Leading- and Trailing-edge Surfaces," Aerospace Science and Technology, Vol. 9, March 2005, pp. 161-171.
  68. Bhoir, N., and Singh, S. N., "Control of Unsteady Aeroelastic System Via State-Dependent Riccati Equation Method," AIAA Journal of Guidance, Control,and Dynamics, Vol. 28, No. 1, January-February 2005, pp. 78-84.
  69. Chemplavil, S., Singh, S.N., and Wells, W.R., "VariableStructure Flutter Control of a Prototypical Wing Section with Unsteady Aerodynamics," Systems Science, Vol. 30, No. 2, 2004, pp. 111-118.
  70. Bhoir, N., and Singh, S. N., "Output Feedback Modular Adaptive Control of a Nonlinear Prototypical Wing Section,"Nonlinear Dynamics, Vol. 37, 2004, pp. 357-373.
  71. Singh, S.N., Simha, A., and Mittal, R., "Birobotic AUV Maneuvering by Pectoral Fins: Inverse Control Design Based on CFD Parameterization," IEEE Journal of Oceanic Engineering, Oct. 2004,pp.777-785.
  72. Gujjula, S., Singh, S. N., Yim, W., "Limit Cycles and Domain of Stability in Unsteady Aeroelastic System," Journal of Guidance,Control, and Dynamics, July-August 2004, pp. 728-732.
  73. Bhoir, N., and Singh, S. N., "Output Feedback Nonlinear Control of an Aeroelastic System WithUnsteady Aerodynamics," Aerospace Science and Technology,Vol. 8, Issue 3, April 2004, pp. 195-205.
  74. Singh, S. N., and Zhang, R., "Adaptive Feedback Control ofSpacecraft with Flexible Appendages by Modeling ErrorCompensation," Acta Astronautica, Vol. 54, No. 4, February 2004,pp. 229-243.
  75. Singh, S. N., Steinberg, M., and Page, A. B., "NonlinearAdaptive and Sliding Mode Flight Path Control of FA-18 Model,"IEEE Transactions on Aerospace and Electronic Systems, Vol. 39, No. 4, pp. 1250-1262, October 2003.
  76. Singh, S. N., and Brenner, M., "Limit Cycle Oscillation andOrbital Stability in Aeroelastic Systems with TorsionalNonlinearity,"Nonlinear Dynamics, Vol. 34, No. 4, pp. 435-450, March 2003.
  77. Singh, S. N., and Brenner, M., "Modular Adaptive Control ofAeroelastic System," Journal of Guidance, Control, and Dynamics, Vol. 25, No. 3, 2003, pp. 443-451.
  78. Chockalingam, F., and Singh, S. N., "Dorsal Fin Control of%Nonminimum Phase Undersea Vehicle Under Surface Waves,"%(Submitted).
  79. Singh, S. N.,Zhang, R., Chandler, P., and Banda, S., "Decentralized Nonlinear Robust Control of UAVs in Close Formation,"International Journal of Robust and Nonlinear Control, Vol. 13, 2003, pp. 1057-1078.%
  80. Singh, S. N., and Yim, W., "State Feedback Controlof anAeroeleastic Systems with Structural Nonlinearity,"AerospaceScience and Technology, Vol. 7, 2003, pp. 23-31.
  81. Yim, W. and Singh S. N., "Adaptive Output Feedback ForceControlof Cantilever Beam Using Piezoelectric Actuator,"Journal of Vibration and Control, Vol. 9, 2003, 567-581.
  82. Singh, S. N., and Wang, L., "Output Feedback Form andAdaptive Stabilization of a Nonlinear Aeroelastic System,"Journal of Guidance, Control, and Dynamics, Jul-Aug 2002, pp. 725-732.
  83. Barone, K, and Singh, S.N., "Adaptive Feedback LinearizingControl of Chua's Circuit,"International Journal of Bifurcation and Chaos, 2002.
  84. Araujo, A., and Singh, S. N., "Output Feedback AdaptiveVariable Structure Control of Chaos in Lorenz System,"International Journal of Bifurcation and Chaos, Vol. 12,No. 3, pp. 571-582, March 2002.
  85. Singh, S. N., Myatt, J., Addington, G., Banda, S., andHall, J."Adaptive Feedback Linearizing Control of ProperOrthogonal Decomposition Nonlinear Flow Models," Nonlinear Dynamics, Vol. 28, 2002, pp. 71-81.
  86. Singh, S. N., Myatt, J., Addington, G., Banda, S., andHall, J., "Optimal Control of Vortex Shedding Using ProperOrthogonal Decomposition Model," ASME Trans. Journal of FluidsEngineering, Vol. 123, No. 3, Sept. 2001, pp. 612-618.
  87. Zhang, R., and Singh, S. N., "Adaptive Output Feedback Controlof an Aeroelastic System with Unstructured Uncertainties," Journal ofGuidance,Control, and Dynamics, Vol. 24, No. 3, pp. 502-509, May-June 2001.
  88. Singh, S. N., Pachter, M, Chandler, P., Banda, S., Rasmessen, S, and Schumacher, C. , "Input-Output Invertibility and Sliding Mode Control for CloseFormation Flying of Multiple UAVs," International Journal ofRobust and Nonlinear Control, Vol. 10, pp. 779-797, 2000.
  89. Singh, S. N., Chandler, P., Banda, S., Schumacher, C., and Pachter, M, "Nonlinear Adaptive Close Formation Control of Unmanned AerialVehicles, Dynamics and Control, Vol. 10, pp. 179-194, 2000.
  90. Yim, W., and Singh, S. N., "Variable Structure AdaptiveForce Tracking Control of a Cantilever Beam Using PiezoelectricActuator," Journal of Vibration and Control, Vol. 6, 2000, pp.1029-1043.
  91. Xing, W., and Singh, S. N., "Adaptive Output Feedback Controlof a Nonlinear Aeroelsatic Structure," Journal ofGuidance,Control, and Dynamics, Nov.-Dec. 2000, pp. 1109-1116.
  92. Xing, W., and Singh, S.N., "Adaptive Control of a NonlinearPrototypical Wing Section with Reduced Order Observer,"Dynamics and Control, Vol. 9, pp. 297-317, 1999.
  93. Bandyopadhyay, P.,Singh, S. N., and Chockalingam, F, "Biologically-Inspired Bodies Under SurfaceWaves Part 2: Theoretical Control of Maneuvering," ASMETransactions Journal of Fluid Engineering, Vol. 121, pp. 479-487, June 1999.
  94. Zeng, Y., Araujo, A., and Singh, S. N., "Output FeedbackVariable Structure Adaptive Control of a Flexible Spacecraft,"Astronautica Acta, Vol. 44, No. 1, pp. 11-22, 1999.
  95. Singh, S. N., and Araujo, A. D. de, "Adaptive Control andStabilization of Elastic Spacecraft," IEEE Transactions onAerospace and Electronic Systems, Vol. 35, pp. 115-122, January1999.
  96. Rivals-Mazeres, G. de., Yim, W., Mora-Camino, F., and Singh,S. N., "Dual Mode Inverse Control and Stabilization of FlexibleSpace Robots," Robotica, Vol. 17, pp. 343-350, 1999.
  97. Zeng, Y., and Singh, S. N., "Output Feedback VariableStructure Adaptive Control of an Aeroelastic Systems," Journal ofGuidance, Control, and Dynamics, Vol 21, No. 6, pp. 830-837,Nov.-Dec. 1998.
  98. Araujo, A. D. de, and Singh, S. N."Variable Structure Adaptive Control of Wing-Rock Motion of Slender Delta Wings," Journal Guidance,Control, and Dynamics, Vol. 21, No. 2, pp. 251-256, March-April 1998.
  99. Zeng Y., and Singh, S. N., "Dynamic Feedback Linearizing Control of Spacecraft with Uncertain Dynamics by SingularPerturbation," Systems Science, Vol. 23, No.3, pp. 79-93, 1997.
  100. Yim, W., and Singh, S. N., "Trajectory Control of FlexibleManipulator Using Rigid Micro Manipulator System," InternationalJournal of Robotics and Automation, Vol. 12, No. 3, pp. 93-99,1997.
  101. Yim, W., and Singh, S. N., "Nonlinear Inverse and PredictiveEnd Point Trajectory Control of Flexible Macro-MicroManipulators," Transaction of ASME Journal of Dynamic Systems,Measurement, and Control, Vol. 119, No. 3, 412-420, Sept 1997.
  102. Singh, S. N., and Bandyopadhyay, P. R., "Linear FeedbackControl of Boundary Layer Using Electromagnetic Microtiles", ASMETransactions Journal of Fluid Engineering, Vol. 119, No. 4, pp.852-858, December 1997.
  103. Singh, S.N., Steinberg, M., and DiGirolamo, R. D., "VariableStructure Robust Flight Control System for the F-14,"IEEE Transactions on Aerospace and Electronic Systems, Vol. 33, No.1, ipp. 77-84, January 1997.
  104. Zeng Y., and Singh, S. N., "Adaptive Control of Chaos in LorenzSystem," Dynamics and Control, Vol. 7, pp. 143-154,1997.
  105. Yim, W., and Singh, S. N., "Predictive End Point TrajectoryControl of Elastic Manipulators," Journal of Robotic Systems,Vol. 13, No. 9, pp. 561-569, Sept. 1996.
  106. Chenumalla, S., and Singh, S. N., "Control of ElasticSpacecraft by Nonlinear Inversion and Singular Perturbation,"The Journal of Astronautical Sciences, Vol. 44, No. 2, pp. 241-262,April-June 1996.
  107. Singh, S.N., and Steinberg, M., "AdaptiveControl of Feedback Linearizable Nonlinear Systems With Applicationto Flight Control," Journal of Guidance, Control, and Dynamics,Vol. 19, No. 4, pp. 871-877, July-August 1996 .
  108. Singh, S., Yim, W., "Feedback Linearization and Solar Pressure Satellite Attitude Control," IEEE Transactions on Aerospace and Electronic Systems, Vol. 32, No.2, pp. 732-741, April 1996.
  109. Chenumalla, S., and Singh, S. N., "Variable Structure EndPoint Control of A Flexible Manipulator," Systems Science, Vol.21, No. 3, pp.83-87., 1995.
  110. Yim, W., and Singh, S. N., "Sliding Mode Force andMotion Control and Stabilization of Elastic Manipulator in ThePresence of Uncertainties,"Journal of Robotic Systems,pp. 315-330, May 1995.
  111. Yim, W., and Singh, S. N., "Inverse Force and Motion Control of Constrained Elastic Robots," ASME Journal of Dynamic Systems, Measurement, andControl, pp. 374-383, Sept. 1995.
  112. Singh, S.N., Steinberg, M., and DiGirolamo, R. D., "NonlinearPredictive Control of Feedback Linearizable Systems and FlightControl System Design," Journal of Guidance, Control, andDynamics, pp. 1023-1028, Sept.-Oct. 1995.
  113. Iyer, A., and Singh, S. N., "Nonlinear Momentum and AttitudeControl of Space Station Accomodating Periodic AerodynamicDisturbance," Acta Astronautica, Vol. 53, No. 6, pp.391-402, 1995.
  114. Singh, S.N., "Output Zeroing Manifold and Nonlinear Regulation ofSpace Station," Systems Science, Vol. 21, N0. 2, 55-62, 1995.
  115. Singh, S., Yim, W., and Wells, W. R., "Direct Adaptive and NeuralControl of Wing-Rock Motion of Slender Delta Wings,"Journal of Guidance, Control, and Dynamics, Vol.18, N0.1,pp.25-30, 1995.
  116. Azam, M., Singh. S.N., Iyer, A., and Kakad, Y.P., "NonlinearRotational Maneuver and Vibration Damping of NASA SCOLE System,"Acta Astronautica, Vol. 32, No. 3, pp. 211-220, 1994.
  117. Singh, S. N., and Iyer, A., "Nonlinear Regulation of Space Station: A Geometric Approach,"Journal of Guidance, Control and Dynamics, Vol. 17, N0. 2,pp.242-249, March-April 1994.
  118. Azam, M., and Singh, S.N., "Nonlinear Invertibility andTrajectory Control for Nonlinear Maneuvers of Aircraft ,"Journal of Guidance, Control, and Dynamics, Vol. 17, No.1,, pp.192-200, January-Feb. 1994.
  119. Yim, W., and Singh, S. N., "Feedback Linearization ofDifferential- Algebraic Systems and Force and Position Control ofManipulators," Dynamics and Control, Vol. 3, No. 4, pp. 323-352, October 1993.
  120. Bossart, T.C., and Singh, S.N., "FeedbackLinearization , Zero Dynamics Stability and Control of Space station Using CMG," Acta Astronautica, ,Vol 29, No. 6, pp.417-427, 1993.
  121. Singh, S. N., and Yim, W., "Sliding Mode Velocity Estimationand Control of Mechanical Manipulators," International Journal ofRobotics and Automation, Vol. 8, N0. 4,pp.188-198, 1993.
  122. Yim, Woosoon, Zuang, J., and Singh, S.N., "ExperimentalTwo-Axis Vibration Control of a Flexible Robotic Arm" ,Journal of Robotic Systems, pp.321-343, 1993.
  123. Madhavan, S., and Singh, S.N., "Variable Structure TrajectoryControl ofAn Elastic Robotic Arm," Journal of Robotic Systems, Vol 10, No.1, pp. 23-44, February 1993.
  124. Singh, S.N., and Bossart, T.C., "Exact Feedback Linearizationand Control of Space Station Using CMG," IEEE Transactions onAutomatic Control, Vol. 38, No. 1, pp.184-187, Jan. 1993.
  125. Singh, S. N., and Wells, W. R., "Adaptive Control ofDecouplable Systems and Nonlinear Flight Control Systems," SystemsScience, Vol. 18, No. 1-2, pp.119-127,1992.
  126. Nathan, P.J., and Singh, S.N., "Nonlinear UltimateBoundedness Control and Stabilization of a Flexible Robotic Arm,"Journal of Robotic Systems, Vol. 9, No. 3, pp.301-326,1992.
  127. Azam, M., Singh. S.N., Iyer, A., and Kakad, Y.P., "Detumblingand Reorientation maneuvers and Stabilization of NASA SCOLESystem," IEEE Transactions on Aerospace and Electronic Systems,Vol. 28, No. 1, pp. 80-91, January 1992.
  128. Yim, Woosoon, Zuang, J., and Singh, S.N., "Experimental DualMode Control of a Flexible Robotic Arm ," Robotica , Vol. 10, pp. 135-145, 1992.
  129. Madhavan, S., and Singh, S.N., "Inverse Trajectory Control and Zero Dynmics Sensitivity of an Elastic Manipulator,"International Journal of Robotics and Automation,Vo. 6. No. 4, pp. 179-192, 1991.
  130. Nathan, P.J., and Singh, S.N., "Sliding Mode Control andElastic Mode Stabilization of a Robotic Arm with Flexible Links,"ASME Transactions Journal of Dynamic Systems, Measurement andControl, December, Vol. 113, pp. 669-676, December 1991.
  131. Iyer A., and Singh, S.N., "Variable Structure SlewingControl and Vibration Damping of Flexible Spacecraft," Astronautica Acta, Vol. 25, No. 1, 1991, pp.1-9..
  132. Romano, J.J., Singh, S.N., "I-O Map Inversion,Zero Dynamics and Flight Control," IEEE Transactions on Aerospace and Electronic Systems, Vol. 25,pp.1022-1029, Nov. 1990.
  133. Das, A. and Singh, S.N., "Nonlinear Adaptive Control andLinear Stabilization of an Elastic Arm," International Journal of Robotics and Automation, Vol. 5, No. 3,PP. 115-123, 1990.
  134. Das, A. and Singh, S.N., "Dual Mode Control of an Elastic Robotic Arm: Nonlinear Inversion and Stabilization by Pole Assignment, " International Journal of Systems Science, Vol. 21, No. 7,pp.1185-1204, 1990.
  135. Wells, W.R, and Singh, S.N., "Asymptotically DecoupledControl and Robust Flight Control System Design," Systems ScienceJournal, Vol. 16, No. 1, pp. 43-66, 1990.
  136. Iyer, A. and Singh, S. N., "Sliding Mode Control of FlexibleSpacecraft under Disturbance Torque, "International Journal ofSystems Science, Vol. 21, No. 9, pp.1755-1771, 1990.
  137. Singh, S.N., "Decoupled Ultimate Boundedness Control ofSystems and Large Aircraft Maneuver," IEEE Transactions onAerospace and Electronic Systems, Vol. 25, 5, 1989, pp.677-688.
  138. Iyer, A. and Singh, S.N., "MFDs of Spinning Satellite and Attitude Control Using Gyrotorquers , " IEEE Transactions on Aerospace and ElectronicSystems, Vol. 25, 5, 1989, pp. 611-620.
  139. Singh, S.N., and Iyer, A., "Nonlinear Decoupling SlidingMode Control and Attitude Control of Spacecraft, "IEEE Transactionsonon aerospace and Electronic Systems, Vol. 25, 5, 1989, pp. 621-633.
  140. Singh, S.N., "Asymptotically Decoupled Discontinuous ofSystems and Nonlinear Aircraft Maneuver, " IEEE Trans. on Aerospace and Electronic Systems, Vol. 25, 1989, pp.380-391.
  141. Singh, S.N., and Zakharia, Y.N., "Variable Structure Control of a Nonlinear Robotic Arm in Presence of Uncertainty, " Journal of Robotic Systems, Vol. 6, No. 2, 1989, pp.111-132.
  142. Singh, S.N., "Control of Nearly Singular Decoupling Systems and Nonlinear Maneuver of Aircraft, "IEEE Trans. on Aerospace and Electronic Systems, Nov. 1988, pp.775-784.
  143. Singh, S.N., "Control of a Nonlinear Uncertain Elastic Arm, "IEEE Transactions on Aerospace and Electronic Systems, Vol.AES-24, No. 2, March 1988, pp.148-155.
  144. Singh, S.N., "Rotational Maneuver of Nonlinear Uncertain Elastic Spacecraft, "IEEE Transactions on Aerospace and Electronic Systems, Vol. AES-24, No. 2, March 1988, pp. 114-123.
  145. Singh, S.N., "Flexible Spacecraft Maneuvers: Inverse Attitude Control and Modal Stabilization, "Acta. Astronautica, Vol. 17,No. 1, 1988, pp. 1-9.
  146. Singh, S.N. and Iyer, A, "Transient Performance of Gyro in Spinning Vehicle, "IEEE Transactions on Aerospace and Electronic Systems, Vol. AES-23, No. 5, Sept. 1987, pp. 620-624.
  147. Singh, S.N., "Attitude Control of Three Rotor Gyrostat in Presence of Uncertainty, " Journal of Astronautical Science,Vol.35, No.3, July-Sept, 1987, pp. 329-345.
  148. Singh, S.N., "Robust Nonlinear Attitude Control of Flexible Spacecraft, "IEEE Transactions on Aerospace and Electronic Systems, Vol. AES-23, No. 3, May, 1987, pp.380-387.
  149. Singh, S.N., "Nonlinear Adaptive Attitude Control of Spacecraft, " IEEE Transactions on Aerospace and Electronic Systems, Vol.AES-23, No. 3, May 1987, pp. 371-379.
  150. Singh, S.N. and Schy, A.A., "Elastic Robot Control: Inversion and Linear Stabilization, "IEEE Transactions on Aerospace and Electronic Systems, Vol. AEs-22, No. 4, July 1986, pp. 340-348.
  151. Singh, S.N., "Nonlinear Attitude Control of Flexible Spacecraft Under Disturbance Torque, "Acta Astronautica, Vol. 13, No. 8, 1986, pp. 507-514.
  152. Mills, C.T.L., Kuruvila, G. and Singh, S.N., "Trajectory Control of PUMA Robot Arm by Inversion and Servocompensation, " International Journal of System Science, Vol. 17, No. 12, 1986, pp. 1709-1725.
  153. Singh, S.N. and Schy, A.A., "Control of Elastic Robotic Systems Nonlinear Inversion and Modal Damping, "ASME TransactionsJournal of Dynamic System Measurement and Control, Vol. 1o8, Sept 1986, pp. 180-189.
  154. Singh, S.N., "Ultimate Boundedness Control of Uncertain Robotic Systems, "International Journal of Systems Science, Vol. 17, No. 6, 1986, pp. 859-863.
  155. Singh, S.N. and Schy, A.A., "Robust Trajectory Following Control of Robotic Systems, "ASME Transactions Journal of Dynamic SystemsMeasurement and Control, Vol.107 , Dec 1985, pp. 308-315.
  156. Singh, S.N., "Adaptive Model Following Control of Nonlinear Robotic Systems, "IEEE Transactions on Automatic Control, Vol.AC-30, N0.11, 1985 , pp.1099-1100.
  157. Singh, S.N.and Coelho, A.R., "Nonlinear Control of Mismatched Uncertain Linear Systems and Application to Control of Aircraft, " ASME Transactions Journal of Dynamic System, Measurement andControl, Sept 1984, pp. 203-210.
  158. Singh, S.N. and Araujo, A.D. de, "Asymptotic Reproducibility in Nonlinear System and Attitude Control of Gyrostat, "IEEE Transactions on Aerospace and Electronic Systems, Vol. AES-20, No. 2, March 1984, pp. 94-103.
  159. Melo, J.D. de and Singh, S.N., "VTOL Aircraft Control Output Tracking Sensitivity Design, "IEEE Transactions on Aerospace and Electronic Systems, Vol. AES- 20, No. 2, March 1984, pp. 82-93.
  160. Singh, S.N., "Gyro Motion Boundedness Under Uncertain Spin and Acceleration of Vehicle, "IEEE Transactions on Aerospace and Electronic Systems, Vol. AES-20, No.2, 1984, pp. 119-127.
  161. Singh, S.N., "Functional Reproducibility in Nonlinear System Using Dynamic Compensation, "IEEE Transactions on Automatic Control, Vol. AC-29, No.5, May 1984, pp. 446-450.
  162. Singh, S.N. and Coelho, A.R., "Ultimate Boundedness Control of Set Points of Mismatched Uncertain Systems, "InternationalJournal of Systems Science, Vol. 14, No. 7, July 1983, pp. 693-710.
  163. Singh, S.N., "Functional Reproducibility and Decouplng Using State Feedback and Dynamic Compensation in Parabolic Distributed Parameter Systems, "International Journal of Systems Science,Vol.14, No.4, 1983, pp. 473-451.
  164. Araujo, A.D. and Singh, S.N., "Asymptotic Functional Reproducibility and Control of Interconnected Power System, "International Journal of Systems Science,Vol. 14, No. 1, 1983, pp. 87-103.
  165. Singh, S.N., "Stability of Gyro with Harmonic Nonlinearity in Spinning Vehicle, "IEEE Transactions on Aerospace and Electronic System, Vol. AES-19, March 1983 , pp. 182-189.
  166. Singh, S.N., "Gyro Motion Boundedness Under Uncertain Acceleration About Vehicle Output Axis, "IEEE Transactions on Aerospace and Electronic Systems, Vol. AES- 12, No.5, Sept. 1982, pp.630-636.
  167. Singh, S.N., "Generalized Functional Reproducibility Condition for Nonlinear Systems, "IEEE Transactions on Automatic ControlVol. AC-27, No. 4, Aug 1982, pp. 958-960.
  168. Singh, S.N., "Reproducibility in Nonlinear Systems Using Dynamic Compensation and Output Feedback, "IEEE Transactions on Automatic Control. Vol. AC-27, Aug 1982, pp.955-958.
  169. Singh, S.N., "Stabilizing Feedback Controls for Nonlinear Hamiltonian Systems and Nonconservative Bilinear Systems in Elasticity, " ASME Trasactions Journal of Dynamic SystemsMeasurement and Control, Vol.104, March 1982 , pp. 27-32.
  170. Singh, S.N., "Functional Reproducibility of Multivariable Nonlinear Systems, "IEEE Transactions on Automatic Control,Vol. AC-27, No. 1, Feb 1982, pp. 270-272.
  171. Singh, S.N., "Invertibility of Observable Multivariable Nonlinear Systems, "IEEE Transactions on Automatic Control, Vol. AC-27,No.2, April 1982, pp. 487-489.
  172. Singh, S.N., "Asymptotically Stable Motions of Gyro in a Spinning Vehicle, "IEEE Transactions on Aerospace and Electronic Systems,Vol. AES-18, No. 1, Jan 1982, pp. 76-81.
  173. Singh, S.N., "Invertibility in Multivariable Parabolic Distributed Parameter Systems, "IEEE Transactions on Automatic Control, Vol. AC-27, No. 1, Feb 1982, pp. 276-279.
  174. Singh, S.N., "Generalized Decoupled Control Synthesis for Invertible Nonlinear Systems, "IEE Proceedings Control Theoryand Applications,Vol. 128, Part D, No. 4, July 1981, pp. 157-161.
  175. Singh, S.N., "A Modified Algorithm for Invertibility in Nonlinear System, "IEEE Transactions on Automatic Control, Vol. AC-26, April 1981, pp. 595-598.
  176. Singh, S.N., "Decoupling of Invertible Nonlinear Systems with State Feedback and Precompensation, "IEEE Transactions on Automatic Control, Vol. AC-25, No. 6, December 1980, pp. 1237-1239.
  177. Singh, S.N., "Stability of a Gyro in a Vehicle Spinning with Uncertain Angular Velocity, "IEEE Transactions on Aerospace and Electronic Systems, Vol. AES-17, No.3, March 1981, pp. 208-212.
  178. Singh, S.N., and Schy, A.A., "Output Feedback Nonlinear Decoupled Control Synthesis and Observer Design for Maneuvering Aircraft, " International Journal of Control, Vol. 31, No. 4, 1980, pp. 781-806.
  179. Singh, S.N., "Nonlinear State Variable Feedback Excitation and Governor Control Design, "IEE Proceedings Control Theory andApplications, Vol. 127, Part D, No.3,May 1980, pp. 131-11.
  180. Singh, S.N., "Single-axis Gyroscopic Motion with Uncertain Angular Velocity about Spin Axis, "Transactions ASME Journal of Dynamic System, Measurement and Control, Dec 1977, pp. 259-267.
  181. Singh, S.N., "Stability of Two Degree of Freedom-Gyro in Spinning Vehicle, "IEEE Transactions on Aerospace and Electronic Systems,Vol. AES-12, July 1976, pp. 514-517.
  182. Singh, S.N., Bhattacharya, L.C., and Rao, C.S., "Measuring Angular Velocity Using Rate Gyro in a Spinning Vehicle, "IEEE Transactions on Aerospace and Electronic Systems, Vol AES-11, Sept 1975, pp. 905-907.
  183. Singh, S.N., "Observability in Nonlinear Systems with Unmeasurable Inputs, "International Journal of SystemsScience, Vol. 6, No. 8, 1975, pp. 723-732.
  184. Singh, S.N., "Decoupling in a Class on Nonlinear Systems by Output Feedback, "Information and Control, Vol. 26,September 1974, pp. 61-81.
  185. Singh, S.N., and Rugh, W.J., "Decoupling in a Class of Nonlinear Systems by State Variable Feedback, "Transactions ASME Journal of Dynamic System, Measurement and Control, Vol. 94, Dec 1972, pp. 323-329.
  186. Singh, S.N., and Rugh, W.J., "Weak Decoupling in Linear and Nonlinear Systems, "Automatica, Vol. 9, 1974, pp. 731-738.
  187. Singh, S.N., and Rugh, W.J., "Decoupling in Linear Time Variable System Using Output Feedback, "International Journal ofControl, Vol. 17, 1973, pp. 321-336.
  188. Sarma, V.V.S., and Singh, S.N., "Comparison of Open and Closed-loop Sensitivities for Systems with Stochastic Inputs, " IEEE Transactions on Automatic Control, Vol. AC-15, April 1970, pp. 253-254.
  189. Sarma, V.V.S., and Singh, S.N., "Controllability and Sensitivity, "IEEE Transactions on Automatic Control, Vol. AC-14, Dec 1969, pp. 782-783.
  190. Singh, S.N., Deekshatulu, B.L., and Sarma, V.V.S., "Singular Optimal Control in Presence of Uncertainty - A Game Theoretic Approach, "International Journal of Control, May 1969, pp. 585-595.
  191. Singh, S.N., Deekshatulu, B.L., and Sarma, V.V.S., "A Differential Game Problem - Plants with Zeroes in Transfer function, "International Journal of Control, May 1969, pp. 577-584.
  192. Singh, S.N., Deekshatulu, B.L., and Sarma, V.V.S., "Game Theoretic Approach to Minimum-effort Control of Second Order System, "International Journal of Control, May 1969, pp. 569-576.

Referred in conferences

  1. Lee, K. W., and Singh, S. N., "MIMO State Prediction Based Adaptive Control of Aeroelastic Systems with Gust Load," International Conference System Engineering (ICSEng2022), Tokyo, August 24, 2022.Applied Systemic Studies - Proceedings of the 29th International Conference onSystems Engineering, ICSEng 2022, Springer.
  2. Lee, K. W., and Singh, S. N., "Adaptive Projectile Fin Control Using Piezoelectric Beam Actuator by $G$-Passification," AIAA Scitech 2022 Forum, AIAA, January 2022.
  3. Lee, K. W., and Singh, S. N., "Composite Adaptive Wing-Rock Control with Regressor Integral Excitation," AIAA Scitech 2022 Forum, AIAA, January 2022.
  4. Lee, K. W., and Singh, S. N., "Chaotic Chua's Circuit's Parameter Estimation Using Composite Identifier and Indirect Adaptive Output Regulation," International Conference System Engineering (ICSEng2021), December 2021, Poland.
  5. Lee, K. W., and Singh, S. N., "Hamiltonian-Based Libration Point OrbitControl on Manifold of Constant Energy," Proceedings of the 27th International Conference on Systems Engineering, ICSEng 2020, year 2021. Springer.
  6. Lee, K. W., and Singh, S. N., "Passification-Based Adaptive Control of Spacecraft withElastic Appendages," AIAA Scitech 2020 Forum, AIAA 2020-1104, January 2020,Orlando, https://doi.org/10.2514/6.2020-1104.
  7. Lee, K. W., and Singh, S. N., "Composite Immersion and Invariance-Based AdaptiveWing-Rock Motion Control," AIAA Scitech 2020 Forum, Paper No. AIAA 2020-0607, January 2020Orlando, https://doi.org/10.2514/6.2020-0607
  8. Lee, K. W., and Singh, S. N., "Generalized Composite Noncertainty-Equivalence Adaptive Control of Orbiting Spacecraft in Vicinity of Asteroid," 2019 AAS/AIAA Astrodynamics Specialist Conference, Portland, ME, Aug. 2019.
  9. Raj, K., Muthukumar, V, and Singh, S. N., "Aircraft Close Formation Control Using Finite-Time Sliding Mode Control Law "(Paper No. AIAA-2019-3180), AIAA AVIATION Forum, San Diego, CA, June 2019. Doi.org/10.2514/6.2019-3180
  10. Moya, N., Lee, K.W., and Singh, S.N., "Adaptive Attitude Control of SpacecraftOrbiting Around Asteroids," 2019 AIAA Guidance, Navigation, and Control Conference, AIAA SciTech Forum, San Diego, CA.,January 6, 2019. doi.org/10.2514/6.2019-0935.
  11. Lee, K.W., and Singh, S.N., "Immersion-and Invariance-Based Adaptive Control of Asteroid-Orbiting and - Hovering Spacecraft," 2018 AAS/AIAA Astrodynamics Specialist Conference, Utah, Aug. 2018.
  12. Raj, K., Muthukumar, V., Singh, S. N., and Lee, K.W., "Robust Higher-Order Sliding Mode Control Systems for Roll-Coupled Maneuvers of Aircraft Using Output Feedback," AIAA AVIATION Forum, (Paper No. AIAA-2018-2833), Atlanta, GA, June 2018.
  13. Lee, K.W., and Singh, S.N., "Robust Higher-Order Super-Twisting Control of Aeroelastic System with Unsteady Aerodynamics," 2018 AIAA Guidance, Navigation, and Control Conference, AIAA SciTech Forum, (AIAA 2018-1341). doi.org/10.2514/6.2018-1341. Gaylord Palms, Kissimmee, Florida, January 8-12, 2018.
  14. Lee, K.W., and Singh, S.N., "Attractive Manifold-Based Noncertainty-Equivalence Adaptive Spacecraft Formation Flying Using Output Feedback," 2018 AIAA Guidance, Navigation, and Control Conference, AIAA SciTech Forum, (AIAA 2018-0865). doi.org/10.2514/6.2018-0865. Gaylord Palms, Kissimmee, Florida, January 8-12, 2018.
  15. Lee, K.W., and Singh, S.N., "Attitude Stabilization of Spacecraft with Flexible Appendages," Proceedings 25th International Conference on Systems Engineering 2017, The Inst. of Elect. and Electronics Enginners, Inc. CA, pp. 3-10.
  16. Lee, K.W., and Singh, S.N., "Super-Twisting Sliding Mode Three-Axis Attitude Control of Spacecraft by Solar Radiation Pressure," AIAA Guidance, Navigation, and Control Conference, AIAA SciTech Forum, (AIAA 2017-1037). doi.org/10.2514/6.2017-1037. Grapevine, TX, January 9-13, 2017.
  17. Ghorawat, P., Lee, K. W., Singh, S. N, and Chmaj, G., "Robust Finite-Time Control of an Uncertain Aeroelastic SystemUsing Leading-and Trailing-Edge Flaps," Advances in Systems Science Volume 539 of the series Advances in Intelligent Systems and Computing, pp 318-328, 2016,DOI: 10.1007/978-3-319-48944-5-29.
  18. Ghorawat, P., Lee, K. W., and Singh, S. N., "Differential Game-Based Control Law for Stabilization of Aeroelastic System with Gust Load," AIAA Guidance, Navigation, and Control Conference, AIAA SciTech, (AIAA 2016-1866), January 2016, San Diego, California. http://dx.doi.org/10.2514/6.2016-1866.
  19. Ghorawat, P., Lee, K. W., and Singh, S. N., "Adaptive Chebyshev Neural Control of a Multi-Input Aeroelastic System Despite Gust Load," AIAA Atmospheric Flight Mechanics Conference, Aviation Forum (AIAA 2015-2555), June 2015, Dallas Texas, (doi: 10.2514/6.2015-2555) .
  20. Lee, K.W., and Singh, S.N., "Solar Pressure Variable Structure Model Reference Adaptive Spacecraft Attitude Control in Elliptic Orbits," AIAA Science and Technology Forum and Exhibition: AIAA Guidance, Navigation, and Control Conference, Baltimore, MD, January 2015.
  21. Srinivasan, L, Lee, K.W., and Singh, S.N., "Robust Output Feedback Attitude Control of Spacecraft Using Solar Radiation Pressure," 23rd International Conference on Systems Engineering,Las Vegas, NV, August 19-21, 2014.
  22. Lee, K.W., and Singh, S.N., "Immersion and Invariance Based Solar Pressure Adaptive Output Feedback Satellite Attitude Control," AIAA Space and Astronautics Forum and Exposition: AIAA/AAS Astrodynamics Specialist Conference, SanDiego, CA., August 2014, doi: 10.2514/6.2014-4102.
  23. Srinivasan, L, Lee, K.W., and Singh, S.N., "Finite-Time Control of Satellites in Elliptic Orbits Despite Uncertainties Using Solar Radiation Pressure," AIAA Science and Technology Forum and Exhibition: AIAA Guidance, Navigation, and Control Conference, Baltimore, MD, January 2014, (doi: 10.2514/6.2014-0448).
  24. Lee, K.W., and Singh, S.N., "Multi-Input Higher-Order Sliding Mode Control of Aeroelastic Systems With Uncertainties and Gust Load," AIAA Science and Technology Forum and Exhibition: AIAA Guidance, Navigation, and Control Conference, Baltimore, MD, January 2014, (doi: 10.2514/6.2014-0603).
  25. Lee, K.W., and Singh, S.N., "Chebyshev Neural Noncertainty-Equivalent Adaptive Control of Wing Rock of Slendar Delta Wings," AIAA Guidance, Navigation,and Control Conference, Boston, MA, August 2013.
  26. Lee, K.W., and Singh, S.N., "Control of a Wing Section Using Leading-and Trailing-Edge Flaps by $L_1$ Adaptive Foodback Despite Disturbances," 51th Aerospace Science Meeting and Exhibit, January 2013, Dallas, TX.
  27. Lee, K.W., and Singh, S.N., "Adaptive Output Feedback Spacecraft Formation Flying Via Observer Based Feedback Linearization," 51th Aerospace Science Meeting and Exhibit, January 2013, Dallas, TX.
  28. Lee, K.W., and Singh, S.N., "Internal Model Principle Based Nonlinear Robust Satellite Formation Control Despite Disturbances," AIAA Guidance, Navigation andControl Conference, Minneapolis, Minnesota, August 2012.
  29. Edosa, D., Lee, K. W., Muthukumar, V., and Singh, S. N., "Hardware-Software Cosimulation of Feedback Controller for Synchronization of Inferior Olive Neurons," The 2012 World Congress in Computer Science, Computer Engineering and Applied Computing (WORLDCOMP'12), MSV, Las Vegas July 2012.
  30. Lee, K.W., and Singh, S.N., "I/O Based Variable Structure Model Reference Adaptive Satellite Formation Control inElliptic Orbits," 50th Aerospace Science Meeting and Exhibit, January 2012, Nashville, TN.
  31. Gutta, S., Singh, S.N. and Yim, W."Adaptive Output Feedback Control of the IPMC Propelled Vehicle with Unknown High Frequency Gain Matrix," ASME 2011 Conference on Smart Materials, Adaptive Structures and Intelligent Systems (SMASIS2011), Scottsdale AZ, Sept 2011.
  32. Lee, K.W., and Singh, S.N., "Output Feedback Variable Structure Adaptive Control Approach to Missile Autopilot", AIAA Guidance, Navigation and Control Conference, Porland, OR, Aug. 2011.
  33. Lee, K. W., Chalike, S. K., Singh, S.N., "Tuning Functions Based Adaptive Synchrony in Inferior Olive Neurons," International Conference on Systems Engineering,August 2011, Las Vegas, NV., pp. 37-42.
  34. Lee, K.W., and Singh, S.N., "Attractive Manifold-based Noncertainty-Equivalent Adaptive Control of Aircraft," 49th Aerospace Science Meeting and Exhibit, January 2011, Orlando, FL.
  35. Lee, K.W., and Singh, S.N., "Noncertainty-Equivalent Adaptive Missile Control via Immersion and Invariance," 48th Aerospace Science Meeting and Exhibit, January 2010, Orlando, FL.
  36. Gutta, S. and Singh, S. N., "Output Feedback Control of Smart Projectile Fin Basedon Internal Model Principle," 2009 ASME Early Career Technical Conference, ASME ECTE, Tuscaloosa, Alabama, October 2009.
  37. Lee, K.W., Ramasamy, S., Singh, S.N., and Selvaraj, H., "Bifurcation%to Periodic Orbits in Inferior% Olive Neurons," Internation Conference on Systems%Engineering, Coventry, England, Sept. 2009.
  38. Lee, K.W. and Singh, S.N., "Noncertainty-EquivalentAdaptive Control of an Aeroelastic System Using Attractive Manifold Design," AIAA Guidance, Navigation, andControl Conference and Exhibit, Chicago, August 2009.%
  39. Lee, K.W., Ramasamy, S., and Singh, S.N., "Adaptive Sliding Mode 3-D Trajectory Control of F/A-18 Model Via SDU Decomposition," AIAA Guidance, Navigation, andControl Conference and Exhibit, Hawaii, Honolulu, August 2008.
  40. Nambisan, P., and Singh, S.N., "Adaptive Control of MIMO Submersibles with Unknown High-Frequency Gain Matrix," International Conference on Systems Engineering, Las Vegas, NV, August 2008.
  41. Lee, K.W., Nambisan, P., and Singh, S.N., "Integrated Adaptive Sliding Mode Controlof Aircraft Using SDU Decomposition of High-Frequency Gain Matrix," 46th Aerospace Science and Exhibit, Paper No. AIAA-2008-0211, January 2008, Reno, NV.
  42. Nambisan, P. and Singh, S.N., "Nonlinear Robust Output FeedbackControl of Submersibles Via Modeling error Compensation," Preceedings of the 16th International Conference on Systems Science, Vol I, pp. 287-296, Sept. 2007, Wroclaw, Poland
  43. Lee, K.W. and Singh, S.N., "Adaptive Control of Spacecraft with Flexible Appendages Using Nussbaum Gain," AIAA Guidance, Navigation, andControl Conference and Exhibit, Paper No. AIAA 2007-6326, pp. 1-12, August 2007,Hilton Head, SC.
  44. Mudupu, V., Singh, S.N., and Yim, W., "AdaptiveControl of a Smart Projectile Fin with Unknown High-Frequency Gain by Piezoelectric Actuation," ASME 2007 International Mechanical Engineering Congress and Exposition, Nov. 2007, Seattle, WA.
  45. Naik, M.S. and Singh, S.N., "Biologically-Inspired Adaptive Pectoral-Like Fin Control System For CFD Parameterized AUV," InternationalSymposium on Underwater Technology, April 2007, Tokyo, Japan, pp. 371-377.
  46. Nambisan, P.R., Singh, S.N., and Wells, W. R., "Robust Control of a Nonlinear Flexible Robot Based on Internal Model Principle," Proceedings of 18th Conference on System Engineering,ICSE 2006, Coventry, UK, Sept. 2006,pp. 319-323.
  47. Mani, S., Singh, S.N., and Yim, W., "Output Feedback Variable Structure Control of a Smart Projectile Fin," AIAA Guidance, Navigation, and Control Conference, Paper No. AIAA 2006-6326, pp. 1-12, August 2006, Keystone, Colorado.
  48. Lee, K.W. and Singh, S.N., "Global Robust Control of an Aeroelastic System Using Output Feedback," AIAA Guidance, Navigation, and Control Conference, Paper No. AIAA 2006-6315, pp. 1-15, August 2006, Keystone, Colorado.
  49. Mani, S., Singh, S.N., Parimi, S., and Yim, W., "Adaptive Servoregulation of a Projectile Fin Using Piezoelectric Actuator, Proceedings of ASME Int. Mechanical Engineering Congress and Exposition (IMECE??05), Nov. 5-11, 2005, Orlando, Florida.
  50. Mani, S., Singh, S.N, Parimi, S.K., Yim, W., Trabia, M., "Direct adaptive control of a smart projectile fin by piezoelectric flexible beam actuator", Proceedings of SPIE Smart Structures and materials 2005: Smart Structure and Integrated Systems, Vol. 5764, pp. 690-702, San Diego, Ca., March 2005.
  51. Maganti, G. B., Subramanian, V, Singh, S.N, and Yim, W., "Modeling and semi-active predictive control of a magnetorheological fluid shock isolation system", Proceedings of SPIE Smart Structures and materials 2005: Damping and Isolation, Vol. 5760, pp. 596-606, San Diego, Ca., March 2005.
  52. Maganti, G, Singh, S.N., and W. Yim, "On Absolute Stability and Semi-active Control of a Magnetorheological Fluid Vibration Suppression System," International Conference on System Engineering, Las Vegas, August 2005.
  53. Gujjula, S. and Singh, S.N., "Variable Structure Control of Unsteady Nonlinear Aeroelastic System with Partial State Information," AIAA Guidance, Navigation, and Control Conference, San Francisco, CA, August 2005.
  54. Mani, S., Singh, S.N., Parimi, S.K., Yim, W., and Trabia, M., "AdaptiveControl of a Piezoelectric Elastic Beam," AIAA Guidance, Navigation, and Control Conference, San Francisco, CA, August 2005.
  55. Renno, J. M., Yim, W., and Singh, S. N., "End Point Position Control of Multi-LinkFlexible Manipulators Using SDRE Method," Proceedings of IMECE ASME International Mechanical Engineering Congress and Exposition, Anaheim, CA., Nov. 20004.
  56. Chemplavil, S., Singh, S.N., Wells, W. R., "Variable Structure Flutter Control of a Prototypical Wing Section with Unsteady Aerodynamics," Proceedings of the XV International Conference on System Science, Vol. I,Wroclaw, Poland, September 2004, pp. 182-189.
  57. Mani, Smitha, Singh, S. N., Parimi, S, Yim, W., and Trabia, M., "AdaptiveTrajectory Control of a Smart Projectile Fin by Piezoelectric Flexible Beam Actuator," Proceedings of International Symposium on Robotics and Automation,Queretaro, Mexico, August 25-27, 2004, pp. 307-312.
  58. Singh. S.N. and Mani. Smitha, "Control of Oscillating Foil for Propulsion of Biorobotic AUV," Proceedings of International Symposium on Robotics and Automation,Queretaro, Mexico, August 25-27, 2004, pp. 145-150.
  59. Gujjula, S., Singh, S. N., and Yim, W., "Limit Cycle Oscillation and Domain of Stability in Prototypical Wing Sections with Unsteady Aerodynamics," AIAA Guidance, Navigation, and Control, August 2004, Providence, RI.
  60. Yim, W., Singh, S. N., M. Trabia, and Drysdale, W., "Adaptive control of smart fin angle using piezoelectric beam actuator," SPIE 11th annual international symposium on Smart Structures and Materials, March 2004, San Diego, CA.
  61. Yim, W., Singh, S. N., and Minnicino, M., "Semi-active control of magnetorheological damper system: Lyapunov approach," SPIE 11th annual international symposium on Smart Structures and Materials, March 2004, San Diego, CA.
  62. Singh, S. N., and Simha, A., "Open-loop and Feedback Pectoral Fin Control of Biorobotic AUV," The 12th International Symposium on Untethered SubmersibleTechnology (UUST03), Durham, NH, August 2003.
  63. Bhoir, N., and Singh, S. N., "Stabilization of anAeroelastic System with Unsteady Aerodynamics: A BacksteppingDesign," AIAA Guidance, Navigation, and ControlConference, Austin, TX, 2003.
  64. Singh, S. N., and Brenner, M., "Limit Cycle Oscillation andOrbital Stability in Aeroelastic Systems with Structural Nonlinearity," International Forum on Aeroelasticity and Structural Dynamics,IFASD, Amsterdam, The Netherlands, June 2003.
  65. Singh, S. N., and Brenner, M., "Modular Adaptive Control ofAeroelastic System," AIAA Guidance, Navigation, and ControlConference, Austin, TX, 2003.
  66. Singh, S. N., and Yim, W., "Nonlinear Adaptive BacksteppingDesign for Spacecraft Attitude Control Using Solar RadiationPressure," Proc. IEEE Conference on Decision and Control, LasVegas, NV., December 2002, pp. 1239-1244.
  67. Yim, W., and Singh, S. N., "End Point Tracking Control ofFlexible Manipulators using SDRE Method," ASME InternationalMechanical Engineering Congress and Exposition, Nov. 2002, Orlando,FL.
  68. Bhoir, N., and Singh, S. N., "Adaptive Angular VelocityEstimation of Three-Axis Vibrating Ring Gyroscope," Proc. of5th International Conference on Systems Engineering, Las Vegas, NV,Aug. 2002, pp. 55-60.
  69. Singh, S. N., and Wang, L., "Output Feedback Form andAdaptive Controlof a Nonlinear Aeroelastic Structure," AIAA Guidance, Navigation,and Control Conference, Monterey, CA, August 2002.
  70. Yim, W., Singh, S. N., and Wells, W. R., "Nonlinear Control of aPrototypical Aeroelastic Wing Section: State-Dependent Riccati Equation Method," submitted to4th International Conference on Non-linear Problems in Aviation andAerospace, Daytona Beach, FL, 2002.
  71. Singh, S. N., Steinberg, M, and Page, A, B., "Variable Structure and Nonlinear Adaptive Flight Control," American Control Conference, Anchorage, Alaska, 2002.
  72. Karmarkar, J., and Singh, S. N., "Adaptive Estimation ofAngular Velocity and Acceleration of a Single-Axis MEMS CoriolisSensor," SPIE Annual International Symposium onSmart Structures and Materials, San Diego, CA, March 2002.
  73. Yim, W., and Singh, S. N., "Robust output feedback control of acantilever beamusing piezoelectric actuator," DSC 13B, 2001 InternationalMechanicalEngineering Conference and Exposition (IMECE) in New York, NY, Nov.2001.
  74. Villaume, F., Fabre, P., Singh, S. N., and Mora-Camino,F., "Control ofInput Redundant Affine Systems: Application to Runway Tracking atLanding," 15th IFAC Symposium on Automatic Control in Space, Bologna, Italy, Sept.2001.
  75. Singh, S. N., Myatt, J., Addington, G., Banda, S., andHall, J."Adaptive Feedback Linearizing Control of ProperOrthogonal Decomposition Nonlinear Flow Models," Proceedings of American Control Conference, Arlington, VA, Vol. 2, pp. 1533-1538, June 2001.
  76. Zhang, R., and Singh, S. N., "Adaptive Output Feedback Controlof Spacecraft with Flexible Appendages," American Control Conference, Arlington, VA, 2001.
  77. Singh, S. N., Zhang, R., M, Chandler, P., Banda, S., "Decentralized Adaptive Close Formation Control," 39th AIAA Aerospace Sciences MeetingandExhibit, Reno, NV, 2001.
  78. Pavan, K., Yim, W., and Singh, S. N., "Adaptive Output Feedback Controlof aFlexible Joint Manipulator," Proceedings of the World AutomationCongress(WAC) 2000, Maui, Hawaii, June 11-15, 2000
  79. Yim, W., Singh, S. N., and Wells, W. R., "Variable Structure AdaptiveWing-StoreFlutter Control by Output Feedback," Proc. of 3rd InternationalConferenceon Non-Linear Problems in Aviation and Aerospace, Dayona Beach, FL,May10-12, 2000.
  80. Schumacher, C., and Singh, S. N., "Nonlinear Control of MultipleUAVs in Close-Coupled Formation Flight," AIAA Gidance, Navigation,and Control Conference, Denver, CO, Paper No. AIAA 2000-4373, Aug. 2000.
  81. Rong, Z., and Singh, S. N., "Robust Output Feedback Controlof an Aeroelastic System Using Modeling Error Compensation," AIAA Guidance, Navigation, and ControlConference, Denver, CO, 2000.
  82. Chockalingam, F., and Singh, S. N., "Dorsal Fin Control ofNonminimum Phase Undersea Vehicle Under Surface Waves," American Control Conference, Chicago, 2000.
  83. Singh, S. N., Pachter, M, Chandler, P., Banda, S., Rasmessen, S, and Schumacher, C., "Input-Output Invertibility and Sliding Mode Control for CloseFormation Flying," AIAA Guidance, Navigation, and ControlConference, Denver, CO, 2000.
  84. Singh, S. N., Chandler, P., Banda, S., Schumacher, C., and Pachter, M, "Adaptive Feedback Linearizing Close Formation Flight Control of UAVs," American Control Conference, Chicago, 2000.
  85. Singh, S.N., Steinberg, M., and DiGirolamo, R. D., "Adaptive%and Variable Structure Lateral Control of the F-14," (Submitted)
  86. Kevin, B., and Singh, S. N., "Adaptive Control of Chaos inChua's Circuit," InternationalConference on Systems Engineering, Las Vegas, EE 1-EE 6 August 1999.%
  87. Xing, W., and Singh, S. N., "Feedback Linearizability andInverse Control of Nonlinear Aeroelastic Systems," InternationalConference on Systems Engineering, Las Vegas, pp. EE241-246, August 1999.
  88. Singh, S. N., Steinberg, M, and Page, A., "Adaptive Control of High-Performance Aircraft with multiple ControlEffectors," AIAA Guidance, Navigation, and Control Conference, Portland, OR,Vol. 3, pp. 1642-1652, August 1999.
  89. Xing, W., and Singh, S. N., "Adaptive Output FeedbackControl of a Nonlinear Aeroelastic Structure," AIAA Guidance, Navigation, and Control Conference, Portland, OR,Vol. 3, 1675-1685, August 1999.
  90. Araujo, A., Singh, S. N., and Wells, W. R., "Output FeedbackNonlinear Discontinuous Adaptive Longitudinal Flight Control formaneuvering Aircraft," Second International Conference onNonlinear Problems in Aviation & Aerospace, NCNPAA-98, Florida., Vol. 1, pp. 9-16, 1998.
  91. Yim, W., and Singh, S. N., "Variable Structure AdaptiveForce Tracking Control of a Cantilever Beam Using PiezoelectricActuator," ASME International Mechanical Engineering Congress, DSC-Vol. 65, Vibration and Noise Control, pp.9-16, 1998.
  92. Zeng, Y., Araujo, A., and Singh, S. N., "Output FeedbackVariable Structure Adaptive Control of a Flexible Spacecraft," AIAA Guidance, Navigation, and Control Conference, Boston, MA.,pp. 383-393, August 1998.
  93. Zeng, Y., and Singh, S. N., "Dynamic Feedback Linearizing Attitude Control ofSpacecraft with Uncertain Dynamics," AIAA Guidance, Navigation, and Control Conference, Boston, MA.,pp. 718-727, August 1998.
  94. Zeng, Y., and Singh, S. N., "Output Feedback VariableStructure Adaptive Control of an Aeroelastic Systems," AIAA Guidance, Navigation, and Control Conference, Boston, MA.,Part2, pp. 522-532, August 1998.
  95. Araujo, A. D. de, and Singh, S. N., "Output Feedback AdaptiveVariable Structure Control of Chaos in Lorenz System," The IFACNonlinear Control Systems Design Symposium (NOLCOS 98), Vol. 3, pp.751-756, Enschede,Holand, July 7, 1998 (also presented in the 12th BrazilianAutomatic Congress, Uberlandia, Minas Gerais, Sept. 1998, Vol. 1,pp. 345-350).
  96. Singh, S. N., and Bandyopadhyay, P. R., "Theoretical ControlStudy of Dive Plane Maneuvering of Small Underwater Vehicles UsingDorsal and Caudal Fins," Bulletineof the American Physical Society, 50th Annual Meeting Division ofFluid Dynamics, San Francisco, C. A., Nov. 1997.
  97. Singh, S.N., Araujo, A. D., and Wells, W.R., "Sliding ModeFlight Control System Design for the F-14," 6th AnnualInternational Conference on Advances in Communication and Control(COMCON VI), Corfu, Greece, June 1997, pp.161-170.Greece, 1997.
  98. Zeng Y., and Singh, S. N., "Dynamic Feedback LinearizingAttitude Control of Spacecraft with Uncertain Dynamics," International Conference on Systems Engineering, Coventry, England, 1997.
  99. Araujo, A. D. de and Singh, S. N., "Variable Structure Adaptive Control ofWing-Rock Motion of Slender Delta Wings," AIAA Atmospheric Flight Mechanics Conference, New Orleans, LA,August 1997.
  100. Singh, S. N., and Araujo, A. D. de, "Adaptive Control andStabilization of Elastic Spacecraft," AIAA Guidance, Navigation and Control Conference, New Orleans, LA,August 1997.
  101. Rivals-Mazeres, G. de., Yim, W., Mora-Camino, F., and Singh,S. N., "Dual Mode Inverse Control and Stabilization of FlexibleSpace Robots," AIAA Guidance, Navigation and Control Conference, New Orleans, LA,August 1997.
  102. Yim, W., and Singh, S. N., "Dynamic Feedback LinearizingForce/Position Control of Robot Manipulation Without VelocityMeasurement," International Conference on Advanced IntelligentMechatoronics, June 1997, Tokyo, Japan.
  103. Singh, S. N., and Bandyopadhyay, P. R., "Feedback TurbulenceControl in Saltwater Using Electromagnetic Microtiles," Bulletineof the American Physical Society, 49th Annual Meeting Division ofFluid Dynamics, Syracuse, N. Y., Nov. 1996.
  104. Singh, S.N., and Steinberg, M., "AdaptiveControl of Feedback Linearizable Nonlinear Systems With Applicationto Flight Control," AIAA Guidance, Navigation, and Control Conference,San Diego, CA, 1996.
  105. Zeng, Y., and Singh, S. N., "Adaptive Control ofMultimachine Power Systems Using Neural Network," 11thInternational Conference on Systems Engineering, Las Vegas, 1996.
  106. Yim, W., and Singh, S. N., "Nonlinear Inverse and PredictiveEnd Point Trajectory Control of Flexible Macro-MicroManipulators," 1996 Int. Federation of Automatic Control,San Francisco, CA.
  107. Yim, W., and Singh, S. N., "Trajectory Control of FlexibleManipulator Using Macro-Micro System," IEEE Conference on Decision and Control, New Orleans, LA., pp.2841-2846, Dec. 1995.
  108. Yim, W., Zeng, Y., and Singh, S. N., "Time Varying TrajectoryControl with Bounded Elastic Modes of FlexibleManipulators," AIAA Guidance, Navigation, and Control Conference,Baltimore, MD, pp. 1503-1509, 1995.
  109. Singh, S. N., Yim, W., and Wells, W. R., "Adaptive FeedbackLinearizing Control of Wing Rock Motion of Slender Delta Wings,International Conf. on Adavances in Communication and Control,1995.
  110. Singh, S.N., Steinberg, M., and DiGirolamo, R. D., "NonlinearPredictive Control of Feedback Linearizable Systems and FlightControl System Design," AIAA Guidance, Navigation, and ControlConference, Baltimore, MD, pp.1084-1093, 1995.
  111. Singh, S.N., Steinberg, M., and DiGirolamo, R. D., "VariableStructure Robust Flight Control System for the F-14," AmericanControl Conference, Seattle, WA, pp. 815-819, June 1995.
  112. Yim, W., and Singh, S. N., "Predictive End-Point TrajectoryControl of Elastic Manipulator," American Control Conference,Seattle, WA, pp.3316-3320, June 1995.
  113. Singh, S., and Yim, W., "Dynamic Feedback Linearization and PitchAttitude Control of Satellite Using Solar Radiation Pressure," American Control Conference, Seattle, WA, pp. 3131-3135, June 1995.
  114. Chenumalla, S., and Singh, S. N., "Control of ElasticSpasecraft by nonlinear inversion and SingularPerturbation," IEEE Conference on Decision and Control, Lake Buena Vista, FL,pp. 927-932, December 1994.
  115. Chenumalla, S., and Singh, S. N., "Inverse and SingularPerturbation Control of Elastic Spacecraft by Velocity Feedback," Proceedings of International System Engineering Conference, Coventry, U .K.,Vol. 1, pp. 185-192, Sept. 1994.
  116. Yim, W., and Singh, S. N., "Sliding Mode Force andMotion Control and Stabilization of Elastic Manipulator in ThePresence of Uncertainties, "Proceedings IEEE InternationalConference on Robotics and Automation, San Diego, CA, pp.2113-2118,1994.
  117. Singh, S., Yim, W., and Wells, W. R., "Adaptive and NeuralControl of Wing-Rock Motion of Slender Delta Wings," Journal of Guidance, Control, and Dynamics, Proceedings 1994 AIAAGuidance, Navigation, and Control,Scottsdale, AZ, pp. 1250-1258, 1994
  118. S. N. Singh, and W. Yim, "Sliding Observer and AdaptiveControl of Robot Manipulators Using Joint Position Feedback," Proceedings of IEEE Conference on Decision and Control, SanAntonio, Texas, pp. 138-141, December 1993.
  119. Singh, S. N., and Wells, W. R., "Nonlinear Adaptive Controlof Flexible Space Structures Using Neural Networks," Proceedingsof Fourth InternationalConference on Advances in Communication and Control, Rhodes,Greece, pp.412-420, June 1993.
  120. Chenumalla, S., and Singh, S. N., "Variable Structure EndPoint Control of Manipulator with Flexible Links," Proceedings ofInternational Conference in Systems Engineering, Las Vegas, NV,pp. 523-527, July 1993.
  121. Singh, S. N.,and Iyer, A., "Output Zeroing Submanifold and Nonlinear Regulation of Space Station : A Geometric Approach," Proceedings of AIAA Guidance, Navigation, and ControlConference, Monterey, CA., pp. 175-185, August 1993.
  122. Chenumalla, S., and Singh, S. N., "Sliding Mode End PointTrajectory Control and Stabilization of Elastic Multi-BodySystem," Proceedings of AIAA Guidance, Navigation, and ControlConference, Monterey, CA., pp. 1482-1491,August 1993.
  123. Iyer, A., and Singh, S. N., "Nonlinear Asymptotic Regulation ofSpace Station Accomodating Periodic Aerodynamic Disturbance," IFAC, Australia, Vol. 5, pp.169-172, 1993.
  124. Yim, W., and Singh, S. N., "Feedback Linearization ofDifferential-Algebraic Systems and Force and Position Control ofManipulators," Proceedings of American Control Conference, San Francisco, pp.2279-2283, June1993.
  125. Yim, W., and Singh, S. N., "Inverse Force/End-Point Control,Zero Dynamics and Stabilization of Constrained Elastic Robots," Proceedings of American Control Conference, San Francisco, pp. 2873-2877, June1993.
  126. Judipi, S., Trabia, B., and Singh, S. N., "Trajectory andVibration Control of a Three-Link Robot Using Inverse JointController and Optimal Multiple Stabilizers," Second Conference on Recent Advances in Active Control of Sound andVibration, VPI, Blacksburg,VA, April 1993, pp.705-716.
  127. Madhavan, S., and Singh, S. N., "Sliding Mode End PointTrajectory Control of a Two Link Elastic Manipulator," Proceedings of IEEEConference on Decision and Control, Tuscon, Arizona, December1992, pp. 305- 310..
  128. Singh, S. N., and Yim, W., "Sliding Mode Velocity Estimationand Control of Mechanical Manipulators," Proceedings of ASMEWinter Annual Meeting, Nov. 1992, Anheim, CA.
  129. Singh, S. N., "Output Zeroing Manifold and NonlinearRegulation of Space Station," International Conference on SystemsScience XI, Wroclaw, Poland, September 1992.
  130. Azam, M., and Singh, S.N., "Invertibility andTrajectory Control for Nonlinear Maneuvers of Aircraft," AIAA Guidance, Navigation and Control Conference, Hilton Head, SC,August 1992.
  131. Azam, M., and Singh, S.N., Iyer, A., and Kakad, Y., "Output Feedback Detumbling and Reorientation Maneuvers of LargeFlexible Structures by Inversion," IEEE Decision and ControlConference, Brighton, U.K., December 1991, pp. 1652-1657.
  132. Singh, S.N., and Bossart, T., "Input-State and Input-OutputFeedback Linearization and Control of Space Station Using CMG," Proceedings of 8th International Conference on System Engineering,Coventry Polytechnic, U.K., Sept. 1991, pp.527-534.
  133. Bossart, T., and Singh, S.N., "Inveribility of Map, ZeroDynamics and Nonlinear Control of Space Station," AIAAGuidance, Navigation and Control Conference, New Orleans, LA., August 1991.
  134. Yim, W., Zuang, J., and Singh, S.N., "Experimental Two-Axis VibrationControl of a Flexible Robot Arm," ASME Winter AnnualMeeting, DSC-Vol. 31,pp. 171-178, Atlanta, GA, Decebmer 1991.
  135. Yim, W., Zuang, J., and Singh, S.N., "Control of a FlexibleRobotic Arm Using PD, Feedforward, and Linear Stabilizer," Fifth International Conference on Advanced Robotics, Pisa, Italy, June1991, pp. 156-161.
  136. Azam, M., and Singh, S.N., Iyer, A., and Kakad, Y., "Feedback Linearization and Control of NASA SCOLE System UsingOutput Feedback," American Control Conference, Boston, MA., June 1991, pp.1038-1043.
  137. Madhavan, S., and Singh, S.N., "Inverse Trajectory Controland Zero Dynamics Sensitivity of an Elastic Manipulator," American Control Conference, Boston, MA., June 1991, pp.1879-1884.
  138. Singh, S.N., and Bossart, T., "Feedback Linearization andNonlinear Ultimate Boundedness Control of Space Station UsingCMG," AIAA Guidance, Navigation and Control Conference, Portland, Oregon,1990, pp. 369-376.
  139. Iyer, A., and Singh, S.N., "Nonlinear Adaptive AttitudeControl of Satellite Using Gyrotorquers," IEEE Conference on Decision and Control, Honolulu, Hawaii, Dec. 1990,pp. 3357- 3361.
  140. Romano, J.J., Singh, S.N., "Inversion of Nonlinear I-O Map,Zero Dynamics, and Flight Control System Design," AIAA Guidance, Navigation and Control Conference, Portland, Oregon,1990, pp. 493- 498.
  141. Das, A. and Singh, S.N., "Dual Mode Nonlinear AdaptiveControl and Stabilization of an Elastic Robotic Arm," IEEEConference on Decision and Control, Honolulu, Hawaii, Dec. 1990,pp. 2659-2660.
  142. Singh, S.N., and Wells, W.R., "Adaptive Control ofDecouplable Systems and Nonlinear Flight Control Systems," International Conference on Systems Engineering, Las Vegas, NV.,1990, pp.235-242.
  143. Nathan, P.J. and Singh, S.N., "Flexible Robotic Arm Control: NonlinearUltimate Boundedness and Linear Stabilization," AmericanControl Conference, San Diego, CA, May 1990, pp.685-690.
  144. Iyer, A., Singh, S.N., "Variable Structure Attitude Controland Elastic Mode Stabilization of a Flexible Spacecraft," IEEE Conference on Decision and Control, Tampa, Florida,December 1989,pp. 809-815.
  145. Singh, S.N., "Ultimate Boundedness Control of UncertainSystems with Application to Roll Coupled Maneuver of Aircraft," IEEE Conference on Decision and Control, Tampa, Florida, December 1989,1708-1713.
  146. Nathan, P.J., Kim, K.I., and Singh, S.N., "Sliding ModeControl of an Elastic Robotic Arm Using Digital Signal Processor," IASTED International Conference Adaptive and Knowledge-BasedControl and Signal Processing, Honolulu,Hawaii, August 1989, pp.24-28.
  147. Das, A., and Singh, S.N., "Dual Mode Control of an Elastic Manipulator: Nonlinear Inversion and Pole Assignment, "American Control Conference, Pittsburgh, PA.,June 1989,pp.1598-1603.
  148. Singh, S.N., "Sliding Mode Asymptotically Decoupled Control and Nonlinear Flight Control System Design, "American Control Conference, Pittsburgh, PA.,June 1989, pp.717-722.
  149. Nathan, P.J., Singh, S.N., "Variable Structure Control of aRobotic Arm with Flexible Links," IEEE International Conference onRobotics and Automation, Scottsdale, AZ.,May 1989, pp.882-887.
  150. Das, A., and Singh, S.N., "Inverse Control and Stabilization:Effect of Coriolis and Centrifugal Force," ISMM InternationalConference, Computer Applications in Design, Simulation andAnalysis, Reno, NV., Feb. 1989, pp. 262-265.
  151. Iyer, A., and Singh, S.N., "Sliding Mode control of Flexible Spacecraft Under Disturbance Torque, "IEEE Conf. on Decision & Control, Austin, TX, Dec. 1988, pp. 718-723.
  152. Singh, S.N., "Decoupling of Systems With Nearly Singular I/O Maps and Application to Nonlinear Control of Aircraft, "IEEE Conf. on Decision & Control, Austin, TX, Dec. 1988, pp. 706-711.
  153. Singh, S.N. and Zakharia, Y.N., "Variable Structure Control of PUMA Arm in Presence of Uncertainty, "International Symposium Robotics and Automation, Santa Barbara, CA., May 1988, pp.104-108.
  154. Iyer, A., and Singh, S.N., "Variable Structure Control of Decoupleable Systems and Attitude Control of Spacecraft in Presence of Uncertainty, "American Control Conference, Atlanta, GA, June 1988, pp. 2238-2243.
  155. Iyer, A., and Singh, S.N., "Minimal Realizations from MFDs and Attitude Control of Spinning Statellite Using Gyrotorquers, "Proceedings of IEEE Conference on Decision and Control, Dec 1987, pp. 1269-1274.
  156. Singh, S.N., "Rotational Maneuver and Stabilization of An Elastic Spacecraft, Proceedings of IEEE Conference on Decision and Control, Dec. 1987, pp.1275-1280.
  157. Singh, S.N., "Controller Design and Dynamic Simulation of Elastic Robot Arm Mounted in Spacecraft in Presence of Uncertainty, "2nd International Conference on Robotic and Factories of Future, July 1987, San Diego, CA, pp. 347-354.
  158. Singh, S.N., "Large Angle Rotational Maneuver of Spacecraft in Presence of University, "5th International Conference on Systems Engineering, Dayton, OH., Sept. 1987, pp. 253-256.
  159. Singh, S.N., "Three Axis Rotational Maneuver and Vibration Stabilization of Elastic Spacecraft, "1987 American Control Conference, Minneapolis, Minnesota, 1106-1110.
  160. Singh, S.N., "Nonlinear Adaptive Control of An Eleastic Robtic Arm, "Proceedings of AIAA Guidance, Navigation, and Control Conference, Williamsburg, VA, Aug. 1986, pp. 28-32.
  161. Singh, S.N., "Model Reference Adaptive Attitude Control of Spacecraft Using Reaction Wheels, "Proceedings of 25th IEEE Conference on Decision and Control, Athens, Greece, Dec. 1986.
  162. Singh, S.N., "Nonlinear Attitude Control of Elastic Spacecraft-Antenna System, "Proceedings of American Control Conference, Seattle, WA, 1986, pp. 1539-1544.
  163. Singh, S.N., "State Variable Feedback Control of a Class of Stochastic Systems, "Proceedings of IEEE Conf oe Decision and Control, Fort Lauderdale, Dec. 1985, pp. 550-551.
  164. Singh, S.N., and Schy, A.A., "Robust Torque Control of an Elastic Robotic Arm Based on Invertibility and Feedback Stabilization, "Proceedings of IEEE Conference on Decision and Control, Fort Lauderdale, Dec. 1985, pp. 1317-1322.
  165. Singh, S.N, and Schy, A.A., "Decomposition and State Variable Feedback Control of Elastic Robotic Systems, "Proceedings of 1985 American Control Conference, Boston, June 1985, pp. 375-380.
  166. Singh, S.N., Mills, C.T.L., and Kuruvila, G., "Nonlinear Generalized Inverse Control of PUMA Robot Arm for Trajectory Reproducibility, 28th Midwest Symposium on Circuits and Systems, Louisville, KY, Aug. 1985, pp. 642-647.
  167. Singh, S.N., "Nonlinear Adaptive Control of Uncertain Robotic Systems, "28th Midwest Symposium on Circuits and Systems, Louisville, KY, Aug 1985,pp. 648-651.
  168. Singh, S.N., "Nonlinear Control of Uncertain Robotic Systems, "Proceedings of International Conference Robotics and Factoryof FutureRobotics and Factories of Future, Charlotte, NC, Dec 1984, pp. 303-309.
  169. Singh, S.N., "Stabilization of a Class of Elastic Systems Using Dynamic Absorbers, "Proceedings of IEEE Conference on Decision and Control, Las Vegas, NV, Dec 1984, pp. 98-99.
  170. Singh, S.N., "Ultimate Boundedness Control of Uncertain Linear Model Following Systems, "Proceedings of IEEE Conference on Decision and Control, Las Vegas, NV, Dec 1984, pp. 1242-1243.
  171. Singh, S.N. and Schy, A.A., "Invertibility and Robust Nonlinear Control of Robotic Systems, "Proceedings of IEEE Conference on Decision and Control, Las Vegas, NV, Dec 1984, pp. 1058-1063.
  172. Singh, S.N., "Robust Control of Robotic System Using Invariance Principle, "Proceedings of Third International Conference on System Engineering, Wright State University, Dayton, Ohio, Sept 1984, pp. 346-353.
  173. Melo, J.D. and Singh, S.N., "Sensitivity Reduction and Robust Tracking with Application to Aircraft Control, "Proceedingsof IEEE Conference on Decision and Control, San Antonio, TX, 1983, pp. 567-572.
  174. Singh, S.N. and Coelho, A.R., "Nonliner State Feedback Control of Uncertain Linear Systems and Application to Control of Aircraft, "Proceedings of IEEE Conference on Decision and Control, San Antonio, TX, 1983, pp. 683-688.
  175. Singh, S.N. and Coelho, A.R., "Control of Uncertain Power System Based on Theory of Ultimate Boundedness, "Proceedings V Chiliean Electrical Engineering Conference, August 1983.
  176. Singh, S.N., "Functional Reproducibility and Right Invertibility in Multivariable Nonlinear Systems, "Proceedings of 4th Brazilian Automatic Control Conference,, 1982, pp. 683-687.
  177. Melo, J.D. and Singh, S.N., "Sensitivity Reduction of Linear System Under Parameter Variation and Disturbance, "VIII AutomaticControl Congress, Buenos Aires, Sept 1982.
  178. Chelho, A.R., Singh, S.N., "On Ultimate Boundedness Control of Aircraft Under Uncertain Parameter Variation, "VIII AutomaticControl Congress,, Buenos Aires, Sept 1982, pp.91-106.
  179. Araujo, A.D., Singh, S.N., "An Inversion Approach to Control of Nonlinear Power System, "Proceedings of 4th Brazilian AutomaticControl Conference, 1982, pp.677-682.
  180. Singh, S.N., "Input-output and Asymptotic Stability of Nonlinear Hamiltonian and Nonconservative System Based on System Topology, "Proceedings of IEEE Conference on Decision and Control, Florida 1982, pp.973-974.
  181. Singh, S.N., "Output Functional Reproducibility and Decoupling Control in Parabolic Distributed Systems, "Proceedings of IEEE Conference on Decision and Control, Florida 1982, pp. 1261-1266..
  182. Araujo, A.D. and Singh, S.N., "Asymptotic Functional Reproducibility and Alert State Steering of Nonlinear Interconnected Power System, "Proceedings of American Control Conference, 1982.
  183. Singh, S.N., "Controller Design for Asymptotic Stability of Flexible Aircraft, "Proceedings of IEEE Conference on Decision and Control, San Diego, CA, Dec 1981, pp. 961-966.
  184. Singh, S.N., "On Asymptotic Stabilization of Nonlinear Hamiltonian Systems and Nonconservative Systems in Elasticity, "Proceedings of IEEE Conference on Decision and Control, San Diego, CA, Dec 1981, pp. 290-295.
  185. Singh, S.N. and Doraiswami, R., "Control of Power System with Multimachines to Obtain Stability Margin, "32 Annual Reunion, SBPC, 1980.
  186. Singh, S.N. and Doraiswami, R., "Nonlinear Load Frequency Control Under Varying Loads, "3rd Brazilian Automatic Control Conference, 1980, pp. 351-356.
  187. Singh, S.N. and Schy, A.A., "Nonlinear Decoupled Control Synthesis for Maneuvering Aircraft, "Proceedings of 17th IEEE Conference on Decision and Control, Jan 1979, pp. 360-370.
  188. Singh, S.N., "Sub-optimal Attitude Transition of Satellite Using Momentum Wheel, "Symposium Yadavapur University, Calcutta, 1976.
  189. Singh, S.N., "Decoupling in Nonlinear Systems, "Symposium on Circuit, System and Computer, Calcutta University, Feb 1975.