Integrated single vs. two loop autopilot-guidance design for dual controlled missiles

@article{Levy2013IntegratedSV,
  title={Integrated single vs. two loop autopilot-guidance design for dual controlled missiles},
  author={Maital Levy and Tal Shima and Shaul Gutman},
  journal={2013 10th IEEE International Conference on Control and Automation (ICCA)},
  year={2013},
  pages={1730-1735}
}
Two types of guidance systems are designed for a dual controlled missile having both forward control and tail control. The first type is an integrated single-loop guidance law, where the coupling between flight control and guidance loops is taken into account in the derivation process. The second type is an integrated two-loop autopilot-guidance law. In… CONTINUE READING