The thesis addresses the problem of multirotors experiencing various disturbances such as wind, payloads and ground effects. These disturbances introduce challenges during specific …
This thesis presents the development, implementation and practical testing of a control system that can automatically land a fixed-wing unmanned aerial vehicle (UAV) onto a …
n this thesis, a flight control system for a quadrotor transporting an unknown suspendedpayload is proposed. The suspended payload parameters, which include its …