Robust adaptive control with reduced conservatism for a convertible UAV

dc.creatorJonatan M. Campos
dc.creatorDaniel Neri Cardoso
dc.creatorGuilherme Vianna Raffo
dc.date.accessioned2025-06-03T14:19:34Z
dc.date.accessioned2025-09-08T23:27:22Z
dc.date.available2025-06-03T14:19:34Z
dc.date.issued2023
dc.identifier.doihttps://doi.org/10.1016/j.ifacol.2023.10.945
dc.identifier.urihttps://hdl.handle.net/1843/82737
dc.languageeng
dc.publisherUniversidade Federal de Minas Gerais
dc.relation.ispartof22nd IFAC World Congress
dc.rightsAcesso Restrito
dc.subjectAeronave não tripulada
dc.subject.otherRobust adaptive control, Convertible UAV, Linear mixed H2/H-infinity control
dc.subject.otherTp model transformation as a way to lmi-based controller design
dc.subject.otherModeling and Robust Control for Full-Flight Envelope Trajectory Tracking of a QuadCP-VTOL Unmanned Aerial Vehicle
dc.subject.otherA robust optimal control approach in the weighted sobolev space for underactuated mechanical systems
dc.titleRobust adaptive control with reduced conservatism for a convertible UAV
dc.typeArtigo de evento
local.citation.epage7
local.citation.spage1
local.description.resumoThis work proposes a robust adaptive mixing controller to achieve trajectory tracking throughout the full-flight envelope, with ensured stability, of a quad-tiltorotor convertible plane (CP) vertical take-off and landing (VTOL) unmanned aerial vehicle (UAV), here called QuadCP-VTOL UAV. Accordingly, a nonlinear multi-body dynamic model is obtained using the Euler-Lagrange formalism, from which a linear parameter-varying (LPV) model is derived to describe the dynamics of the QuadCP-VTOL UAV within its flight envelope. The set containing the UAV's flight envelope is partitioned into subsets and, for each subset, a less conservative formulation of the linear robust mixed H2/H∞ candidate controller is proposed. An adaptive mixing scheme is employed to perform a convex combination of the candidate controllers within the subsets intersection. Results of Hardware-In-the-Loop (HIL) experiments are presented to corroborate the efficacy of the proposed control strategy.
local.publisher.countryBrasil
local.publisher.departmentENG - DEPARTAMENTO DE ENGENHARIA ELÉTRICA
local.publisher.departmentENG - DEPARTAMENTO DE ENGENHARIA ELETRÔNICA
local.publisher.initialsUFMG
local.url.externahttps://www.sciencedirect.com/science/article/pii/S2405896323013289

Arquivos

Licença do pacote

Agora exibindo 1 - 1 de 1
Carregando...
Imagem de Miniatura
Nome:
License.txt
Tamanho:
1.99 KB
Formato:
Plain Text
Descrição: