Vývoj kombinovaného leteckého přístroje pro experimentální a ultralehká letadla

Abstract

The bachelor thesis deals with the complex development of a combined aeronautical device intended for use in experimental and ultralight aircraft. This includes the careful selection and design of hardware such as sensors to monitor attitude, speed and other important aircraft parameters, a suitable display to present the data to the pilot and powerful processors to process the information in real time. The development also includes the detailed creation of a display layout that will be able to effectively interpret the sensor data and provide useful information to the pilot. Another important aspect is the integration of the proposed avionics into specific aircraft types. This includes the physical installation of the components in the aircraft and interfacing with existing systems. To ensure the reliability and functionality of the proposed avionics, tests and verifications will be carried out under different operating conditions, including simulation of faults and failures. The aim of the whole process is to create advanced avionics that will be affordable and bring innovation to the field of avionics for experimental and ultralight aircraft.