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008 220407t20212021my a|||fram|| 001 0 eng d
020 _aTHE0009299(Local)
040 _aUMP
_beng
_cUMP
_erda
090 _aFTKEE .B35 2021 r Thesis
100 0 _aBalya Darohini,
_eauthor.
245 1 0 _aOptimizing performance on a quaternion based quadrotor control scheme /
_cBalya Darohini
264 1 _aKuantan, Pahang :
_bUMP ;
_c2021
264 4 _aΒ© 2021
300 _axii, 89 pages :
_billustrations (some color) ;
_c30 cm. +
_e1 CD ROM
336 _atext
_2rdacontent
337 _aunmediated
_2rdamedia
338 _avolume
_2rdacarrier
347 _atext file
_bPDF
_2rda
500 _aFaculty of Electrical & Electronics Engineering
502 _aThesis (Master of Science) -- Universiti Malaysia Pahang – 2021
504 _aIncludes bibliographical references
520 3 _aQuadrotor has become very popular and their usage has spread over all fields of life that require some demanded tasks. The demanded tasks for Quadrotor to be complicated require the control algorithms to have better performance and more efficiency. Thus, comprehensive aim precisely at the development of control algorithm for quadrotor based on a hybrid of controller synthesis on Proportional Integral Derivative (PID) and Proportional Controller, π‘ƒπœ” so that the performance and functionality system may be compromised. This project started with the modeling of the dynamics Quaternion angle based on quadrotor since Euler’s angle is prone to gimbal lock. This led to the implementation of the quadrotor in a computer simulation environment called Simulink. Then followed by the hybrid of controller synthesis on PID and π‘ƒπœ” implemented in the dynamic Quaternion model. The proposed hybrid control algorithm and quadrotor attitude model have been implemented in fully Quaternion space without any conversion and calculations in the Euler’s angles. In this project, the optimized Quaternion composed of 𝐾𝑃, 𝐾𝐼 , 𝐾𝐷 and π‘ƒπœ” are proposed, and finally, the output effective waveform produced by optimization using Genetic Algorithm and Particle Swarm Optimization are shown and presented by simulations using MATLAB. The efficiency of the proposed scheme has been proven after using optimized gain of 𝐾𝑃 , 𝐾𝐼 , 𝐾𝐷 and π‘ƒπœ” and presented thoroughly. It has shown that the proposed Quaternion angle based on Quadrotor control scheme has a better response as they can cater the error with a very good and fast-tracking in step response analysis about 1.3s than 4.2s shown in previous work whereas about 31% of improvement. For sin wave response, the following error has been reduced from Β±40% to Β±0.02%. For ramp response, it improvised the response to follow the reference accordingly without shifted up or shifted down from the reference. Plus, it has proven there is zero overshoot produce by the optimized system and the proposed controller allowing a good attitude of control over its Roll, Pitch, and Yaw angles.
610 2 0 _aFaculty of Electrical & Electronics Engineering Technology
_xDissertations
650 0 _aUniversities and colleges
_xDissertations
650 0 _aTheses
942 _2lcc
_cRESTRICT