Dynamic Inversion-Enhanced U-Control of Quadrotor Trajectory Tracking

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Dynamic Inversion-Enhanced U-Control of Quadrotor Trajectory Tracking. / Lone, Ahtisham; Zhu, Quanmin; Nemati, Hamidreza et al.
In: Drones, Vol. 8, No. 10, 599, 18.10.2024.

Research output: Journal contributionsJournal articlesResearchpeer-review

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Lone A, Zhu Q, Nemati H, Mercorelli P. Dynamic Inversion-Enhanced U-Control of Quadrotor Trajectory Tracking. Drones. 2024 Oct 18;8(10):599. doi: 10.3390/drones8100599

Bibtex

@article{b433a27e4e604977b972cad8e34a373f,
title = "Dynamic Inversion-Enhanced U-Control of Quadrotor Trajectory Tracking",
abstract = "This study proposes a universal (U)-control enhanced with dynamic inversion for a class of multiple-input multiple-output (MIMO) quadrotor flight tracking operations. In the technique, a robust compensator is integrated with the U-controller to achieve stabilisation at the equilibrium and setpoint tracking in the presence of any unmodelled uncertainties and external disturbances. A series of bench tests of simulated and real experiments on a Parrot Mambo quadrotor are conducted to show the design framework from the academic formulation to Simulink simulation and real flight tests.",
keywords = "quadrotor control, quadrotor UAV, simulation and flying tests, trajectory tracking, U-dynamic inversion, U-model realisation, Engineering",
author = "Ahtisham Lone and Quanmin Zhu and Hamidreza Nemati and Paolo Mercorelli",
note = "Publisher Copyright: {\textcopyright} 2024 by the authors.",
year = "2024",
month = oct,
day = "18",
doi = "10.3390/drones8100599",
language = "English",
volume = "8",
journal = "Drones",
issn = "2504-446X",
publisher = "MDPI AG",
number = "10",

}

RIS

TY - JOUR

T1 - Dynamic Inversion-Enhanced U-Control of Quadrotor Trajectory Tracking

AU - Lone, Ahtisham

AU - Zhu, Quanmin

AU - Nemati, Hamidreza

AU - Mercorelli, Paolo

N1 - Publisher Copyright: © 2024 by the authors.

PY - 2024/10/18

Y1 - 2024/10/18

N2 - This study proposes a universal (U)-control enhanced with dynamic inversion for a class of multiple-input multiple-output (MIMO) quadrotor flight tracking operations. In the technique, a robust compensator is integrated with the U-controller to achieve stabilisation at the equilibrium and setpoint tracking in the presence of any unmodelled uncertainties and external disturbances. A series of bench tests of simulated and real experiments on a Parrot Mambo quadrotor are conducted to show the design framework from the academic formulation to Simulink simulation and real flight tests.

AB - This study proposes a universal (U)-control enhanced with dynamic inversion for a class of multiple-input multiple-output (MIMO) quadrotor flight tracking operations. In the technique, a robust compensator is integrated with the U-controller to achieve stabilisation at the equilibrium and setpoint tracking in the presence of any unmodelled uncertainties and external disturbances. A series of bench tests of simulated and real experiments on a Parrot Mambo quadrotor are conducted to show the design framework from the academic formulation to Simulink simulation and real flight tests.

KW - quadrotor control

KW - quadrotor UAV

KW - simulation and flying tests

KW - trajectory tracking

KW - U-dynamic inversion

KW - U-model realisation

KW - Engineering

UR - http://www.scopus.com/inward/record.url?scp=85207652960&partnerID=8YFLogxK

UR - https://www.mendeley.com/catalogue/51dc60a2-cd73-3427-a3fe-333dfbaca581/

U2 - 10.3390/drones8100599

DO - 10.3390/drones8100599

M3 - Journal articles

AN - SCOPUS:85207652960

VL - 8

JO - Drones

JF - Drones

SN - 2504-446X

IS - 10

M1 - 599

ER -

DOI