@inproceedings{9de5908cc8ca4c9ea87b214b668a031b,
title = "L1 adaptive output feedback controller for non strictly positive real reference systems with applications to aerospace examples",
abstract = "This paper presents an extension of the L1 adaptive output feedback controller to systems of unknown relative degree in the presence of time-varying uncertainties without restricting the rate of their variation. As compared to earlier results in this direction, a new piece-wise continuous adaptive law is introduced along with the low-pass filtered control signal that allows for achieving arbitrarily close tracking of the input and the output signa{\l} of the reference system, the transfer function of which is not required to be strictly positive real (SPR). Stability of this reference system is proved using small-gain type argument. The performance bounds between the closed-loop reference system and the closed-loop L1 adaptive system can be rendered arbitrarily small by reducing the step size of integration. Simulations verify the theoretical findings.",
author = "Chengyu Cao and Naira Hovakimyan",
note = "Copyright: Copyright 2020 Elsevier B.V., All rights reserved.",
year = "2008",
doi = "10.2514/6.2008-7288",
language = "English (US)",
isbn = "9781563479458",
series = "AIAA Guidance, Navigation and Control Conference and Exhibit",
publisher = "American Institute of Aeronautics and Astronautics Inc.",
booktitle = "AIAA Guidance, Navigation and Control Conference and Exhibit",
}