Sliding Mode Control of VTOL System

Jacob, Jerry

dc.contributor.author	Jacob, Jerry
dc.coverage.spatial	Coimbatore
dc.date.accessioned	2022-10-11T22:33:59Z
dc.date.available	2022-10-11T22:33:59Z
dc.date.issued	2019-11-06
dc.identifier.citation	(2019, April 12-13). [Conference item]. First International Conference on Materials Science and Manufacturing Technology 12–13 April 2019, Hotel Aloft, Coimbatore, Tamil Nadu, India, Coimbatore.
dc.identifier.uri	https://hdl.handle.net/2292/61555
dc.description.abstract	QUANSER QNET 2.0 Vertical Take Off and Landing (VTOL) system is a hardware device setup developed by National Instruments to study flight dynamics and vertical take-off and landing control. It has a DC Motor fan and adjustable counter weight. This is used exclusively for NI-ELVIS platform and LabVIEW software. The LabVIEW software is used to identify the model of the system by the method of best fit. The obtained second order model is tested for the open loop response using MATLAB SIMULINK. The various control methods like Proporional+Integral+Velocity (PIV) and Sliding Mode Control (SMC) are used to find the response of the system. It is found that the sliding mode controller provides better results compared to the PIV controller. Along with this, the actuator control is done using PI controller and it's response along with the system is analyzed and compared for both PIV and Sliding Mode Controller.
dc.description.uri	https://www.researchgate.net/publication/337197832_Sliding_Mode_Control_of_VTOL_System
dc.relation.ispartof	First International Conference on Materials Science and Manufacturing Technology 12–13 April 2019, Hotel Aloft, Coimbatore, Tamil Nadu, India
dc.relation.ispartofseries	Sliding Mode Control of VTOL System
dc.rights	Items in ResearchSpace are protected by copyright, with all rights reserved, unless otherwise indicated. Previously published items are made available in accordance with the copyright policy of the publisher.
dc.rights.uri	https://researchspace.auckland.ac.nz/docs/uoa-docs/rights.htm
dc.rights.uri	https://creativecommons.org/licenses/by/3.0/
dc.title	Sliding Mode Control of VTOL System
dc.type	Conference Item
pubs.volume	561
dc.date.updated	2022-09-08T00:06:53Z
dc.rights.holder	Copyright: The authors	en
pubs.author-url	https://iopscience.iop.org/article/10.1088/1757-899X/561/1/012069
pubs.finish-date	2019-04-13
pubs.start-date	2019-04-12
dc.rights.accessrights	http://purl.org/eprint/accessRights/OpenAccess	en
pubs.subtype	Conference Paper
pubs.elements-id	918234
pubs.org-id	Engineering
pubs.org-id	Department of Electrical, Computer and Software Engineering
pubs.record-created-at-source-date	2022-09-08
pubs.online-publication-date	2019-11-06