Nature inspired based pitch controller design of an UAV

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dc.contributor.authorJada, C.
dc.contributor.authorPaul, K.
dc.contributor.authorOmkar, S.N.
dc.contributor.authorTutika, S.
dc.date.accessioned2026-02-05T09:35:06Z
dc.date.issued2012
dc.description.abstractIn this paper a longitudinal control system has been designed for a 2 Kg payload Unmanned Aerial Vehicle using classical PID controller. To overcome the difficulty in tuning the PID gains to the required values, different nature inspired techniques have been used, for the Integral Squared Error (ISE) parameter optimization on UAV dynamic data at a specified trim condition. For this purpose, the penalty function that has been chosen includes time domain specifications as constraints. Finally all the results are compared for optimum PID parameters.
dc.identifier.citationInternational Journal of Aerospace Innovations, 2012, 3, 4, pp. 217-231
dc.identifier.issn17572258
dc.identifier.urihttps://doi.org/10.1260/1757-2258.3.4.217
dc.identifier.urihttps://idr.nitk.ac.in/handle/123456789/26909
dc.subjectDynamic data
dc.subjectGSO
dc.subjectIntegral squared error
dc.subjectParameter optimization
dc.subjectPenalty function
dc.subjectPID controllers
dc.subjectPID gains
dc.subjectPID parameters
dc.subjectPitch controller
dc.subjectPSO
dc.subjectTime-domain specifications
dc.subjectFlight control systems
dc.subjectFlight dynamics
dc.subjectGallium
dc.subjectLongitudinal control
dc.subjectRoot loci
dc.subjectThree term control systems
dc.subjectUnmanned aerial vehicles (UAV)
dc.subjectControllers
dc.titleNature inspired based pitch controller design of an UAV

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