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Attitude control of tiltwing aircraft using a wing-fixed coordinate system and incremental nonlinear dynamic inversion
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In
International journal of micro air vehicles 11, Seiten/Artikel-Nr.:1-12
2019
Online
DOI: 10.18154/RWTH-2019-09817
DOI: 10.1177/1756829319861370
URL: https://publications.rwth-aachen.de/record/770930/files/770930.pdf
Einrichtungen
Thematische Einordnung (Klassifikation)
DDC: 380
OpenAccess: 
PDF
Dokumenttyp
Journal Article
Format
online, print
Sprache
English
Anmerkung
Peer reviewed article
Externe Identnummern
SCOPUS: SCOPUS:2-s2.0-85073555554
WOS Core Collection: WOS:000490135500001
OpenAlex: W2980611696
Interne Identnummern
RWTH-2019-09817
Datensatz-ID: 770930
Beteiligte Länder
Germany
Related:
Contribution to a conference proceedings
Attitude Control of Tiltwing Aircraft Using a Wing-Fixed Coordinate System and Incremental Nonlinear Dynamic Inversion
[10th International Micro-Air Vehicles Conference, IMAV2018, 2018-11-17 - 2018-11-23, Melbourne, Australia]
10. International Micro-Air Vehicles Conference, IMAV 2018, MelbourneMelbourne, Australia, 17 Nov 2018 - 23 Nov 2018
(2018)
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