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Robust Flight Control Design for the FASER UAV

Weiser, Christian (2017) Robust Flight Control Design for the FASER UAV. Master's, Technische Universität München.

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In-flight demonstration and verification of a robust flight control design in-cluding an advanced anti-windup strategy is presented in this thesis. The test aircraft, an Ultrastick 120 unmanned aircraft, is provided with a pitch- and roll-attitude command flight-control system for remotely controlled augment-ed flight. The longitudinal aircraft dynamics are enhanced with an

Item URL in elib:https://elib.dlr.de/118400/
Document Type:Thesis (Master's)
Title:Robust Flight Control Design for the FASER UAV
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Weiser, ChristianChristian.Weiser (at) dlr.deUNSPECIFIED
Date:December 2017
Refereed publication:No
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Keywords:Robust Control, Flight Control, UAV
Institution:Technische Universität München
Department:Flugzeug System Dynamic
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Systems and Cabin (old)
Location: Oberpfaffenhofen
Institutes and Institutions:Institute of System Dynamics and Control > Aircraft System Dynamics
Deposited By: Pusch, Manuel
Deposited On:22 Jan 2018 14:41
Last Modified:22 Jan 2018 14:41

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