Integrated Guidance and Control of Missiles With$theta hbox - D$Method

  title={Integrated Guidance and Control of Missiles With\$theta hbox - D\$Method},
  author={Ming Xin and S. N. Balakrishnan and E. J. Ohlmeyer},
  journal={IEEE Transactions on Control Systems Technology},
A new suboptimal control method is proposed in this study to effectively design an integrated guidance and control system for missiles. Optimal formulations allow designers to bring together concerns about guidance law performance and autopilot responses under one unified framework. They lead to a natural integration of these different functions. By modifying the appropriate cost functions, different responses, control saturations (autopilot related), miss distance (guidance related), etc… CONTINUE READING
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Publications referenced by this paper.
Showing 1-10 of 18 references

Integrated design of agile missile guidance and control systems

  • P. K Menon, E. J Ohlmeyer
  • Proc. 7th Mediterranean Conf. Contr. Autom., 1999…
  • 1999
Highly Influential
6 Excerpts

Optimal controller for homing missiles

  • C. F. Lin, W. R. Yueh
  • J. Guid., Contr., Dynamics, vol. 8, no. 3, pp…
  • 1985
Highly Influential
3 Excerpts

A new method for suboptimal control of a class of nonlinear systems

  • M. Xin, S. N Balakrishnan
  • Opt. Contr. Appl. Methods, vol. 26, no. 2, pp. 55…
  • 2005
2 Excerpts

Nonlinear missile autopilot design with theta-D technique

  • M. Xin, S. N Balakrishnan, D. T Stansbery, E. J Ohlmeyer
  • AIAA J. Guid. Control Dyn., vol. 27, no. 3, pp…
  • 2004
1 Excerpt

Integrated guidance-control system of a homing interceptor: sliding mode approach

  • I. Shkolnikov, Y. Shtessel
  • presented at the AIAA Guid. Nav. Contr. Conf…
  • 2001
1 Excerpt

Nonlinear integrated guidance and control laws for homing missiles

  • P. K. Menon, E. J. Ohlmeyer
  • presented at the AIAA Guid., Nav. Contr. Conf…
  • 2001
3 Excerpts

Nonlinear integrated guidance and control laws for homing missiles , ” presented at the AIAA Guid . , Nav . Contr . Conf . Exhibit , Montreal , ON , Canada , Aug .

  • G. D Sweriduk P. K Menon, E. J Ohlmeyer, D. S. Malyevac
  • J . Guid . Control Dyn .
  • 2001

Control of a continuously stirred tank reactor using an asymmetric solution of the state-dependent Riccati equation

  • J. R Cloutier, D. T Stansbery
  • Proc. IEEE Conf. Contr. Appl., 1999, pp. 893–898.
  • 1999
1 Excerpt

Integrated missile guidance and control: A state dependent Riccati differential equation approach

  • N. F Palumbo, T. D Jackson
  • Proc. IEEE Int. Conf. Contr. Appl., 1999, pp. 243…
  • 1999
1 Excerpt

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