@inproceedings{7ec4d2ffee3a48f2b24394dd38602b83,
title = "Design examples: Adaptive tracking control in the presence of input constraints for a fighter aircraft and a generic missile",
abstract = "Two flight control related examples of adaptive autopilot design in the presence of actuator constraints are presented. The demonstrated methodology maintains closed-loop stability by changing guidance commands on-line. In addition, the method is capable of avoiding control saturation at all times, if required.",
author = "Amir Ajami and Naira Hovakimyan and Eugene Lavretsky",
year = "2005",
doi = "10.2514/6.2005-6444",
language = "English (US)",
isbn = "1563477378",
series = "Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference",
publisher = "American Institute of Aeronautics and Astronautics Inc.",
pages = "5916--5924",
booktitle = "Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference 2005",
note = "AIAA Guidance, Navigation, and Control Conference 2005 ; Conference date: 15-08-2005 Through 18-08-2005",
}