U-model-based dynamic inversion control for quadrotor UAV systems

Research output: Contributions to collected editions/worksChapterpeer-review

Standard

U-model-based dynamic inversion control for quadrotor UAV systems. / Aziz Lone, Ahtisham; Nemati, Hamidreza; Zhu, Quanmin et al.

Modeling, Identification, and Control for Cyber- Physical Systems Towards Industry 4.0. Elsevier, 2024. p. 293-309.

Research output: Contributions to collected editions/worksChapterpeer-review

Harvard

Aziz Lone, A, Nemati, H, Zhu, Q, Mercorelli, P & Narayan, P 2024, U-model-based dynamic inversion control for quadrotor UAV systems. in Modeling, Identification, and Control for Cyber- Physical Systems Towards Industry 4.0. Elsevier, pp. 293-309. https://doi.org/10.1016/B978-0-32-395207-1.00025-1

APA

Aziz Lone, A., Nemati, H., Zhu, Q., Mercorelli, P., & Narayan, P. (2024). U-model-based dynamic inversion control for quadrotor UAV systems. In Modeling, Identification, and Control for Cyber- Physical Systems Towards Industry 4.0 (pp. 293-309). Elsevier. https://doi.org/10.1016/B978-0-32-395207-1.00025-1

Vancouver

Aziz Lone A, Nemati H, Zhu Q, Mercorelli P, Narayan P. U-model-based dynamic inversion control for quadrotor UAV systems. In Modeling, Identification, and Control for Cyber- Physical Systems Towards Industry 4.0. Elsevier. 2024. p. 293-309 doi: 10.1016/B978-0-32-395207-1.00025-1

Bibtex

@inbook{2465a7553e9642caacb071a10413d341,
title = "U-model-based dynamic inversion control for quadrotor UAV systems",
abstract = "A Model-Independent Design approach (U-Model) is studied with the example of Quadrotor UAV. A Multiple-Input Multiple-Output (MIMO) dynamic model of a quadrotor UAV is derived, and U-Model-based Dynamic Inverse control approach is used to design a controller, which is made of two parts. The first part consists of a general controller designed independently to guarantee the performance requirements defined in advance. Secondly, this independent controller is then integrated with the inverse of the model. In this chapter, we consider a Parrot Mambo Minidrone as a research subject to simulate and validate the controller performance. The simulations results are presented at the end with graphical illustrations demonstrating the effectiveness of the proposed controller.",
keywords = "MIMO control, Quadrotor control, U-model dynamic inversion (UM-DI), U-model-based controller",
author = "{Aziz Lone}, Ahtisham and Hamidreza Nemati and Quanmin Zhu and Paolo Mercorelli and Pritesh Narayan",
note = "Publisher Copyright: {\textcopyright} 2024 Elsevier Inc. All rights reserved.",
year = "2024",
month = jan,
day = "1",
doi = "10.1016/B978-0-32-395207-1.00025-1",
language = "English",
isbn = "9780323952088",
pages = "293--309",
booktitle = "Modeling, Identification, and Control for Cyber- Physical Systems Towards Industry 4.0",
publisher = "Elsevier",
address = "France",

}

RIS

TY - CHAP

T1 - U-model-based dynamic inversion control for quadrotor UAV systems

AU - Aziz Lone, Ahtisham

AU - Nemati, Hamidreza

AU - Zhu, Quanmin

AU - Mercorelli, Paolo

AU - Narayan, Pritesh

N1 - Publisher Copyright: © 2024 Elsevier Inc. All rights reserved.

PY - 2024/1/1

Y1 - 2024/1/1

N2 - A Model-Independent Design approach (U-Model) is studied with the example of Quadrotor UAV. A Multiple-Input Multiple-Output (MIMO) dynamic model of a quadrotor UAV is derived, and U-Model-based Dynamic Inverse control approach is used to design a controller, which is made of two parts. The first part consists of a general controller designed independently to guarantee the performance requirements defined in advance. Secondly, this independent controller is then integrated with the inverse of the model. In this chapter, we consider a Parrot Mambo Minidrone as a research subject to simulate and validate the controller performance. The simulations results are presented at the end with graphical illustrations demonstrating the effectiveness of the proposed controller.

AB - A Model-Independent Design approach (U-Model) is studied with the example of Quadrotor UAV. A Multiple-Input Multiple-Output (MIMO) dynamic model of a quadrotor UAV is derived, and U-Model-based Dynamic Inverse control approach is used to design a controller, which is made of two parts. The first part consists of a general controller designed independently to guarantee the performance requirements defined in advance. Secondly, this independent controller is then integrated with the inverse of the model. In this chapter, we consider a Parrot Mambo Minidrone as a research subject to simulate and validate the controller performance. The simulations results are presented at the end with graphical illustrations demonstrating the effectiveness of the proposed controller.

KW - MIMO control

KW - Quadrotor control

KW - U-model dynamic inversion (UM-DI)

KW - U-model-based controller

UR - http://www.scopus.com/inward/record.url?scp=85189596142&partnerID=8YFLogxK

U2 - 10.1016/B978-0-32-395207-1.00025-1

DO - 10.1016/B978-0-32-395207-1.00025-1

M3 - Chapter

AN - SCOPUS:85189596142

SN - 9780323952088

SP - 293

EP - 309

BT - Modeling, Identification, and Control for Cyber- Physical Systems Towards Industry 4.0

PB - Elsevier

ER -