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

@article{Xin2006IntegratedGA,
  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},
  year={2006},
  volume={14},
  pages={981-992}
}
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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