The paper presents the design and performance of the flight stabilisation system onboard computer developed in Łukasiewicz Research Network – Institute of Aviation. The presented unit is an electronic block performing automatic flight stabilisation of an aeroplane using trimmers. It was designed based on the launch platform PZL-130 Orlik aircraft requirements. The article contains the unit’s hardware and software design description, unit performance, tests results and conclusions with improvements possibilities.
Hardware and Software Design of Onboard Computer Controlling the Flight Stabilisation System
Advs in Intelligent Syst., Computing
Conference on Automation ; 2022 ; Warsaw, Poland May 25, 2022 - May 27, 2022
Automation 2022: New Solutions and Technologies for Automation, Robotics and Measurement Techniques ; Chapter : 13 ; 126-132
2022-04-16
7 pages
Article/Chapter (Book)
Electronic Resource
English