Sliding Mode Control of VTOL System

Show simple item record

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


Files in this item

Find Full text

This item appears in the following Collection(s)

Show simple item record

Share

Search ResearchSpace


Browse

Statistics