Show simple item record

dc.contributor.authorMuhammad Kamran, Joyo
dc.date.accessioned2016-11-29T09:04:12Z
dc.date.available2016-11-29T09:04:12Z
dc.date.issued2013
dc.identifier.urihttp://dspace.unimap.edu.my:80/xmlui/handle/123456789/44204
dc.description.abstractIn recent years the area of quadrotor UAV has drawn prominent attention of the researchers enabling to develop immense research area in the field of UAVs. A quadrotor has a simple architectural design due to which designing gets simple. Having advantage of uniqueness in shape and simple design it carries numerous kinds of issues regarding its controlling. A quadrotor system is nonlinear in nature, so it requires a suitable controller to ensure its stability during flight. However, researchers have been able to provide some solutions to the issues regarding angular stability, altitude and position control of quadrotor under the challenging conditions such as wind burst and noisy measurements but still they are not successfully resolved. In this thesis report modern control design techniques are discussed and their application in quadrotor control issues are presented. The control techniques are implemented on a longitudinal motion control of quadrotor i.e. issues related while maneuvering on horizontal plane. After imposing few renowned control techniques on the system it was observed that system requires to build a robust control technique for the quadrotor system. An innovative and more robust control technique is proposed for the position controlling quadrotor system. The controller is designed by fusing two distinct control techniques PID and LQR, which is named as PID-LQR. While flying quadrotor can experience two major issues; noises and external disturbance applied on the system. The nature of noises is the noise generated from GPS sensor and the system itself. The nature of disturbance is the disturbance applied externally on the system. The control technique works in such a way that PID is used for tackling a disturbance such as an external push or wind gust and LQR for rejecting noises of the sensor measurements. Furthermore the effectiveness of proposed control technique is also verified by comparing it with autotuned PID and optimized LQR techniques under disturbed and noisy conditions. The simulated results indicate that the proposed method yields a better response as compared to the conventional methods.en_US
dc.language.isoenen_US
dc.publisherUniversiti Malaysia Perlis (UniMAP)en_US
dc.subjectControl algorithm (PID-LQR)en_US
dc.subjectQuadrotor UAVen_US
dc.subjectPID controllersen_US
dc.subjectPoint-to-Point (PTP)en_US
dc.subjectLQR Controlleren_US
dc.subjectUnmanned aerial vehicles (UAV)en_US
dc.titleDevelopment of control algorithm (PID-LQR) for point to point movement of a nonlinear quadrotor unmanned aerial vehicleen_US
dc.typeLearning Objecten_US
dc.contributor.advisorProf. Madya Dr. Hazry Desaen_US
dc.publisher.departmentSchool of Mechatronic Engineeringen_US


Files in this item

Thumbnail
Thumbnail

This item appears in the following Collection(s)

Show simple item record