About S Balakrishnan

Education

  • University Of Texas Austin, Doctor of Philosophy, 1984

S Balakrishnan

Curators distinguished profess
Mechanical & Aerospace Engin
271 Toomey Hall

573-341-4675 | bala@mst.edu | Personal site

Education

  • University Of Texas Austin, Doctor of Philosophy, 1984

Research

Research interests

Guidance, stability, control and estimation, pattern recognition, stochastic processes, optimization, neural network applications to control, numerical methods and design.

Publications

  • Xin, Ming and Balakrishnan, S.N., "Missile Longitudinal Autopilot Design Using A New Suboptimal Nonlinear Control
    Method" IEE Proceedings Control Theory and Applications, Vol. 150, No.6, Nov. 2003,
    pp.577-584.
  • Prabhat, P., Look, D.C., and Balakrishnan, S.N., "Experimental Model determination for Neurocontrol of a Thermal Conduction
    System" AIAA Journal of Thermal Physics and Heat Transfer, Vol. 17, No.4, October
    December 2003, pp. 471-480.
  • Padhi, R. and Balakrishnan, S.N., "Proper Orthogonal Decomposition based Optimal Neurocontrol Synthesis of a
    Chemical Reactor Process Using Approximate Dynamic Programming" Neural
    Networks, , Vol. 16, 2003, pp. 719-728.
  • Padhi, R. and Balakrishnan, S.N., "Development and Analysisof a Feedback Treatment Strategy for Parturient Paresis
    of Cows," IEEE Transactions on Control Systems Technology, Vol. 12, No. 1, January,
    2004, pp.52-64.
  • Xin, M. and Balakrishnan, S.N., "Control of Wing Rock Motion Using a New Suboptimal Control Method,"Proceedings
    of the IMECH, Journal of Aerospace Engineering, Vol. 218, pp. 257-266.
  • Xin, M. and Balakrishnan, S.N., Stansbery, D. and Ohlmeyer, E., "Nonlinear Bank-to-Turn/Skid-to-Turn Missile Outer-Loop/Inner-Loop Autopilot
    Design with the Technique" AIAA Journal of Guidance, Control and Dynamics, Vol. 27,
    No.3, May-June, 2004, pp. 406-417.
  • Han, D., Balakrishnan, S.N. and Ohlmeyer, E.J., "Midcourse Guidance Law with Neural Networks," accepted for publication in Journal
    of Aerospace Engineering.
  • Hu, Z. and Balakrishnan, S.N., "Parameter Estimation in Nonlinear Systems Using Hopfield Neural Networks," AIAA
    Journal of Aircraft, Vol. 42, no.1, Jan.-Feb. 2005,pp. 41-53.
  • Panurangan, B., Landers, R. and Balakrishnan, S.N., "Hierarchical Optimal Force-Position Control of a Turning Process," accepted for
    publication in IEEE Transactions on Control Systems Technology.
  • Drake, D. T. and Balakrishnan, S.N., "Theta-D Control Technique for Ascent Control of Reusable Launch Vehicles," AIAA
    Journal of Guidance, Control, and Dynamics, Vol. 27, No.6, Nov-Dec. 2004, pp. 938-
    948.
  • Drake, D.T. and Balakrishnan, S.N., "Theta-D Technique for Control of Aeroelastic Flutter," submitted to IEEE Proceedings
    on Control Theory and Applications.
  • Padhi, R. and Balakrishnan, S.N., Optimal Beaver Population Management Using Reduced Order Distibuted Parameter
    Model and Single Network Adaptive Critics," accepted for publication inIEEE
    Transactions on Control System Technology.
  • Padhi, R., Prabhat, P. and Balakrishnan, S.N., "Reduced Order Optimal Control Synthesis of a Class of Nonlinear Distributed
    Parameter Systems Using Single Network Adaptive Critics," submitted to Soft
    Computing Journal.
  • Xin, M. Balakrishnan , S.N. and Ohlmeyer, E., "Integrated Guidance and Control of Missiles with Method," accepted for publication
    in IEEE Transactions on Control System Technology.

Course information