Design and development of optimal control system for quad copter uav

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dc.contributor.authorTahir, Zaid
dc.contributor.authorJamil, Mohsin
dc.contributor.authorLiaqat, S Ali
dc.contributor.authorMubarak, Lubva
dc.contributor.authorTahir, Waleed
dc.contributor.authorGilani, Syed Omer
dc.date.accessioned2023-12-14T05:41:45Z
dc.date.available2023-12-14T05:41:45Z
dc.date.issued2016
dc.descriptionA quad copter is a multi-rotor UAV that uses four rotors to lit itself of the ground. As the name ‘quad’ suggests.
dc.description.abstractDesign and development of an optimal control system for a quadcopter unmanned aerial vehicle (UAV). The 6DOF quad copter state-space models was used for Linear Quadratic Regulator (LQR) and Linear Quadratic Gaussian (LQG) simulations in MATLAB/Simulink. The simulations produced satisfactory results, which have been presented. A comparison between Low Pass Filter (LPF) and Kalman filter is also shown which shows that LQR is useless in presence of noise hence LQG was employed in such a situation. The optimal control system for quadcopter was successfully developed, which can be practically implemented on an actual quadcopter for stable unmanned flight of the aerial vehicle. Keywords: Control, DOF, GPS, LQR, LQG, LPF, Quad-Copter, UAV
dc.identifier.citationTahir, Z., Jamil, M., Liaqat, S. A., Mubarak, L., Tahir, W., & Gilani, S. O. (2016). Design and development of optimal control system for quad copter uav. Indian Journal of Science and Technology, 9(25), 10-17485.
dc.identifier.doihttps://doi.org/10.17485/ijst/2016/v9i25/96611
dc.identifier.urihttps://dspace.adu.ac.ae/handle/1/236
dc.language.isoen
dc.publisherResearchGate
dc.titleDesign and development of optimal control system for quad copter uav
dc.typeArticle

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