2021
DOI: 10.1049/cth2.12137
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A combined model reference adaptive control law for multirotor UAVs

Abstract: Model reference adaptive control (MRAC) offers the potential to adapt in real-time to changes in the performance of small unmanned air vehicles. There are significant challenges with their use, however, primarily in the implementation and assurance of long-term system stability. This paper presents flight test results for a combined model reference adaptive control (CMRAC) law applied to the height control loop of a multirotor. Key features include the implementation of CMRAC with a baseline controller allowin… Show more

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Cited by 9 publications
(7 citation statements)
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References 50 publications
(84 reference statements)
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“…Meanwhile, [36] considered an adaptive control law with a known input matrix substituted by its estimate. Lastly, [37,38] neglected the estimation error and considered an unknown input matrix to control uncrewed underwater and air vehicles, respectively. Hence, this manuscript uses the ideas originally proposed by CMRAC [31][32][33] to extend the D adaptive-passivity-based control (APBC) technique [30], which is ensure faster results than MRAC for the IFOC scheme.…”
Section: Of 20mentioning
confidence: 99%
“…Meanwhile, [36] considered an adaptive control law with a known input matrix substituted by its estimate. Lastly, [37,38] neglected the estimation error and considered an unknown input matrix to control uncrewed underwater and air vehicles, respectively. Hence, this manuscript uses the ideas originally proposed by CMRAC [31][32][33] to extend the D adaptive-passivity-based control (APBC) technique [30], which is ensure faster results than MRAC for the IFOC scheme.…”
Section: Of 20mentioning
confidence: 99%
“…A model reference adaptive system (MRAS) method was also demonstrated in [22] to estimate the position and speed of permanent magnet synchronous motor (PMSM) by considering the error between the real and the estimated rotor position values. Flight test results were presented in [23] for a combined model reference adaptive control (CMRAC) law applied to the height control loop of a multirotor. In [24], a new leakage-based mechanism was designed for robust adaptive control of uncertain switched systems: in contrast to the available designs, the key innovation of the proposed one was that the adaptive gains of the inactive subsystems can be kept constant to their switched-off values, thus preventing vanishing gains.…”
Section: Introductionmentioning
confidence: 99%
“…Recently, many other novel height controllers have been designed for multirotor UAVs, considering disturbances in different scenarios. A combined model reference adaptive control law is given for height control loop of a multirotor [24]. An adaptive nonsingular fast terminal SMC strategy is introduced to realize height control for quadrotors with variable mass and external disturbance [25].…”
Section: Introductionmentioning
confidence: 99%