Design and analysis of a novel l1 adaptive controller, part i: control signal and asymptotic stability

C Cao, N Hovakimyan - 2006 American Control Conference, 2006 - ieeexplore.ieee.org
In this paper, we develop a novel adaptive control architecture that ensures that the input
and output of an uncertain linear system track the input and output of a desired linear system …

Augmented L1 adaptive tracking control of quad-rotor unmanned aircrafts

Z Zuo, P Ru - IEEE Transactions on Aerospace and Electronic …, 2014 - ieeexplore.ieee.org
This paper addresses a new trajectory tracking controller for quad-rotor aircrafts in the
presence of time-varying aerodynamic effect and bounded external disturbance using the …

Design and analysis of a novel L1 adaptive controller, Part II: Guaranteed transient performance

C Cao, N Hovakimyan - 2006 American Control Conference, 2006 - ieeexplore.ieee.org
In this paper, we present a novel adaptive control architecture that ensures that the input and
output of an uncertain linear system track the input and output of a desired linear system …

L1 adaptive control design for NASA AirSTAR flight test vehicle

I Gregory, C Cao, E Xargay, N Hovakimyan… - … , navigation, and control …, 2009 - arc.aiaa.org
In this paper we present an extension of the L1 adaptive control architecture to nonlinear
systems in the presence of significant uncertain cross-coupling. To evaluate the L1 adaptive …

L1 adaptive control augmentation system for the X-48B aircraft

T Leman, E Xargay, G Dullerud… - … , navigation, and control …, 2009 - arc.aiaa.org
Verification and Validation (V&V) of gain-scheduled flight control systems relies on analysis
of gain and phase margins across the flight envelope. Because similar tools are not …

Adaptive fuzzy controller for a class of nonlinear systems with unknown backlash-like hysteresis

HA Yousef, M Hamdy, K Nashed - International Journal of Systems …, 2017 - Taylor & Francis
This paper proposes an adaptive fuzzy logic control scheme for a class of strict-feedback
nonlinear systems with unknown backlash-like hysteresis. The proposed controller exploits …

Flight Test of an L (sub 1) Adaptive Controller on the NASA AirSTAR Flight Test Vehicle

IM Gregory, E Xargay, C Cao… - … Guidance, Navigation and …, 2010 - ntrs.nasa.gov
This paper presents results of a flight test of the L-1 adaptive control architecture designed to
directly compensate for significant uncertain cross-coupling in nonlinear systems. The flight …

L1 adaptive controller for multi-input multi-output systems in the presence of nonlinear unmatched uncertainties

E Xargay, N Hovakimyan, C Cao - Proceedings of the 2010 …, 2010 - ieeexplore.ieee.org
This paper presents the L 1 adaptive controller for a class of multi-input multi-output
nonlinear systems in the presence of unmatched uncertainties. The L 1 controller ensures …

Evolution of flying qualities analysis: Problems for a new generation of aircraft

MC Cotting - 2010 - vtechworks.lib.vt.edu
A number of challenges in the development and application of flying qualities criteria for
modern aircraft are addressed in this dissertation. The history of flying qualities is traced …

Adaptive Output Feedback Controller for Systems of Unknown Dimension

C Cao, N Hovakimyan - IEEE Transactions on Automatic …, 2008 - ieeexplore.ieee.org
This note presents novel adaptive output feedback control methodology for systems of
unknown dimension in the presence of unmodeled dynamics and time-varying uncertainties …