Go to:
Logótipo
Comuta visibilidade da coluna esquerda
Você está em: Start > Publications > View > Automatic Circular Take-off and Landing of Motorized Tethered Aircraft
Publication

Publications

Automatic Circular Take-off and Landing of Motorized Tethered Aircraft

Title
Automatic Circular Take-off and Landing of Motorized Tethered Aircraft
Type
Article in International Conference Proceedings Book
Year
2024
Authors
Vinha, S
(Author)
Other
The person does not belong to the institution. The person does not belong to the institution. The person does not belong to the institution. Without AUTHENTICUS Without ORCID
Fernandes, GM
(Author)
Other
The person does not belong to the institution. The person does not belong to the institution. The person does not belong to the institution. Without AUTHENTICUS Without ORCID
Nguyen, HT
(Author)
Other
View Personal Page You do not have permissions to view the institutional email. Search for Participant Publications View Authenticus page Without ORCID
Fernandes, MCRM
(Author)
Other
The person does not belong to the institution. The person does not belong to the institution. The person does not belong to the institution. Without AUTHENTICUS Without ORCID
Conference proceedings International
Pages: 681-686
European Control Conference (ECC)
Stockholm, SWEDEN, JUN 25-28, 2024
Indexing
Other information
Authenticus ID: P-016-T4R
Abstract (EN): We consider a motorized aircraft tethered to a central anchorage point in a configuration similar to a control line model airplane. For this system, we address the problem of automatic take-off and landing (ATOL) with a circular path, whose center and radius are defined by the anchorage point and the tether length, respectively. We propose a hierarchical control architecture for ATOL and discuss the controllers designed for each control layer and for each of the flight phases. Simulation results are reported, showing the viability of the approach, but also showing the limitations on the maximum altitude attainable with a fixed-tether length. The tethered aircraft and the proposed ATOL control architecture are to be used in an Airborne Wind Energy System.
Language: English
Type (Professor's evaluation): Scientific
No. of pages: 6
Documents
We could not find any documents associated to the publication.
Related Publications

Of the same authors

Control of Fixed-Wing Tethered Aircraft in Circular Take-Off and Landing Maneuvers (2024)
Article in International Conference Proceedings Book
Vinha, S; Fernandes, GM; Fernandes, MCRM; Nguyen, HT; Fontes, Fernando A C C
Recommend this page Top
Copyright 1996-2025 © Faculdade de Direito da Universidade do Porto  I Terms and Conditions  I Acessibility  I Index A-Z
Page created on: 2025-10-22 at 18:50:56 | Privacy Policy | Personal Data Protection Policy | Whistleblowing | Electronic Yellow Book