AIAA Guidance, Navigation, and Control Conference 2012
DOI: 10.2514/6.2012-4831
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L1 Adaptive Controller for Attitude Control of Multirotors

Abstract: In this work we show an application of L1 Adaptive control theory for attitude control of UAVs. We implement the flight control system on a multirotor to show robustness and precise attitude tracking in the presence of modeling uncertainties and environmental disturbances. We choose backstepping control architecture, since the kinematics and dynamics of multirotors in most cases can be written in strict feedback form. We further exploit the fact that the kinematics of the plant, while free of uncertainties, is… Show more

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Cited by 45 publications
(30 citation statements)
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References 7 publications
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“…This promotes a very fast adaptation rate while keeping the control input sufficiently smooth, making L 1 a much more practical adaptive control technique [6], [2]. L 1 attitude controllers have been developed for attitude control of quadrotors, using Euler angles (or quaternions) as attitude states [25], [19], [5], [17] or for general linear sys-tems [4]. Geometric adaptive schemes have been previously developed for quadrotor control in [14], [12].…”
Section: A Related Workmentioning
confidence: 99%
“…This promotes a very fast adaptation rate while keeping the control input sufficiently smooth, making L 1 a much more practical adaptive control technique [6], [2]. L 1 attitude controllers have been developed for attitude control of quadrotors, using Euler angles (or quaternions) as attitude states [25], [19], [5], [17] or for general linear sys-tems [4]. Geometric adaptive schemes have been previously developed for quadrotor control in [14], [12].…”
Section: A Related Workmentioning
confidence: 99%
“…This allows arbitrarily high adaptation gains to be chosen for fast adaptation and to determine uniform bounds for the system's state and control signals [5]. Attitude control based on L 1 adaptive control was shown in [6], where three algorithms were successfully implemented and tested on a quadrotor, hexacopter and octocopter, respectively. L 1 adaptive output feedback on translational velocity was successfully implemented on a quadrotor to compensate for artificial reduction in the speed of a single motor [7].…”
Section: Introductionmentioning
confidence: 99%
“…This algorithm has been successfully implemented on UAVs to augment a baseline controller for improved disturbance rejection. Attitude control based on L 1 adaptive control was shown in [8], where three algorithms were successfully implemented and tested on a quadrotor, hexacopter and octocopter, respectively. In [9], L 1 adaptive control is implemented for a quadrotor in translational velocity output feedback control, and shows the ability of the controller to compensate for artificial reduction in the speed of a single motor.…”
Section: Introductionmentioning
confidence: 99%