@inproceedings{5007545493cd449a840e5f86050d92ec,
title = "Integrated single vs. two loop autopilot-guidance design for dual controlled missiles",
abstract = "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 this case, the autopilot loop is designed separately from the guidance one, but all the states are fed-back into the guidance loop. It is demonstrated that the integrated two-loop autopilot-guidance law can manipulate the inner autopilot dynamics, resulting in the same performance as the integrated single-loop guidance law. The performance of the integrated two-loop autopilot-guidance diagram is shown to be highly dependent on the chosen autopilot block diagram.",
author = "Maital Levy and Tal Shima and Shaul Gutman",
year = "2013",
doi = "10.1109/ICCA.2013.6564961",
language = "الإنجليزيّة",
isbn = "9781467347075",
series = "IEEE International Conference on Control and Automation, ICCA",
pages = "1730--1735",
booktitle = "2013 10th IEEE International Conference on Control and Automation, ICCA 2013",
note = "2013 10th IEEE International Conference on Control and Automation, ICCA 2013 ; Conference date: 12-06-2013 Through 14-06-2013",
}