elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Contact | Deutsch
Fontsize: [-] Text [+]

Robust Flight Control Design for the FASER UAV

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

Full text not available from this repository.

Abstract

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
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Weiser, ChristianChristian.Weiser (at) dlr.deUNSPECIFIED
Date:December 2017
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
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
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

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
electronic library is running on EPrints 3.3.12
Copyright © 2008-2017 German Aerospace Center (DLR). All rights reserved.