Modelling the dynamics and control system of hybrid airship UAV (HAU-3)

In this thesis, a 3.3 m length, finless hull airship called HAU-3 is presented. Four vector thrusters arranged in H-Frame configurations were attached to the hull, which enable the airship to maneuver in 5DOF. To allow a deeper understanding of the HAU-3 motion behavior and to design a flight contro...

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Détails bibliographiques
Auteur principal:	Sedan, Mohd Fazri
Format:	Thèse
Langue:	anglais
Publié:	2022
Sujets:	Airships Flight control Hybrid airplanes
Accès en ligne:	http://psasir.upm.edu.my/id/eprint/104091/1/MOHD%20FAZRI%20BIN%20SEDAN%20-%20IR.pdf

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