Please use this identifier to cite or link to this item: https://idr.l1.nitk.ac.in/jspui/handle/123456789/6741
Full metadata record
DC FieldValueLanguage
dc.contributor.authorJamadagni, C.S.
dc.contributor.authorChethan, C.U.
dc.contributor.authorJeppu, Y.V.
dc.contributor.authorKamble, S.B.
dc.contributor.authorDesai, V.H.
dc.date.accessioned2020-03-30T09:46:03Z-
dc.date.available2020-03-30T09:46:03Z-
dc.date.issued2014
dc.identifier.citationProceedings of 2014 International Conference on Contemporary Computing and Informatics, IC3I 2014, 2014, Vol., , pp.404-408en_US
dc.identifier.urihttp://idr.nitk.ac.in/jspui/handle/123456789/6741-
dc.description.abstractThis paper discusses an approach for system simulation of an autopilot system designed for a Bell helicopter model. The flight controls for the helicopter is designed in Matlab/Simulink and the same is visualized in X-Plane flight simulator. The approach involves software in loop simulation method where controls are designed in Matlab/Simulink and the responses are observed on X-Plane plant. The interaction between the Matlab/Simulink and X-Plane is through UDP. A parameter identification of the X-Plane model is carried out from data obtained through UDP. This simulation setup is a good way to learn the intricacies of systems development, plant identification and control. � 2014 IEEE.en_US
dc.titleSystem simulation approach for helicopter autopiloten_US
dc.typeBook chapteren_US
Appears in Collections:2. Conference Papers

Files in This Item:
There are no files associated with this item.


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.