Hybrid unmanned aerial vehicle modeling and control

In the test study, a hybrid unmanned aerial design was designed and the modeling and control development of this design was studied. Designed as both rotary wing and fixed wing, this unmanned aerial vehicle can fly in the desired form thanks to its vtol landing and take-off capability. In line with the analysis, mechanical tests and avionics tests, it is stated in which direction the study will reach the result. In line with the designs made, it was decided to make the body of balsa, taking into account the criteria of being light and durable. It was decided to make it from wing and tail balsa material due to its economic, light and workability. Mechanical parts were drawn in solidworks program and analyzed in ansys program. Autopilot module Pixhawk Cube Orange was used to perform autonomous flight in the created system. Thanks to this module used, DC motor controls in the system, reading of telemetry data and processing of radio control signals are carried out. The telemetry module used in the system is RFD900+, and it instantly transmits parameters such as speed, altitude, pressure, temperature of the unmanned aerial vehicle in flight to the ground station.