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Incremental Nonlinear Dynamic Inversion Flight Control implementation and flight test on a fixed wing UAV

Vlaar, Cornelis Mattheus (2014) Incremental Nonlinear Dynamic Inversion Flight Control implementation and flight test on a fixed wing UAV. Master's, Delft University of Technology.

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Item URL in elib:https://elib.dlr.de/105670/
Document Type:Thesis (Master's)
Title:Incremental Nonlinear Dynamic Inversion Flight Control implementation and flight test on a fixed wing UAV
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Vlaar, Cornelis MattheusUNSPECIFIEDUNSPECIFIED
Date:2014
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:134
Status:Published
Keywords:nonlinear dynamic inversion, flight controller
Institution:Delft University of Technology
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: Klauer, Monika
Deposited On:12 Aug 2016 11:12
Last Modified:12 Aug 2016 11:12

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