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dc.contributor.authorKava, Sean Anthony
dc.contributor.supervisorProf. Khac Duc Doen_US

Despite the fact that aerodynamic loads (forces and moments) induced by airflow relative to a quadrotor vertical take-off and landing aircraft consist of both deterministic and stochastic components, all existing works on controlling the aircraft either ignore these loads or treat them as deterministic. This simplification deteriorates the control performance in a practical implementation. This thesis presents a constructive design of controllers for a quadrotor aircraft to track a reference path in three-dimensional space under both deterministic and stochastic aerodynamic loads.

dc.publisherCurtin Universityen_US
dc.titleDynamics and Control of a Multi-Rotor Aircraften_US
curtin.departmentMechanical Engineeringen_US
curtin.accessStatusOpen accessen_US
curtin.facultyScience and Engineeringen_US

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