Aircraft Automatic Control Systems and their Control Systems
Róbert Bréda
; Technical University of Košice Faculty of Aeronautics Slovakia
František Adamčík
; Technical University of Košice, Faculty of Aeronautics Slovakia
APA 6th Edition Bréda, R. i Adamčík, F. (2014). Aircraft Automatic Control Systems and their Control Systems. NAŠE MORE, 61 (1-2), S9-12. Preuzeto s https://hrcak.srce.hr/121592
MLA 8th Edition Bréda, Róbert i František Adamčík. "Aircraft Automatic Control Systems and their Control Systems." NAŠE MORE, vol. 61, br. 1-2, 2014, str. S9-12. https://hrcak.srce.hr/121592. Citirano 22.01.2021.
Chicago 17th Edition Bréda, Róbert i František Adamčík. "Aircraft Automatic Control Systems and their Control Systems." NAŠE MORE 61, br. 1-2 (2014): S9-12. https://hrcak.srce.hr/121592
Harvard Bréda, R., i Adamčík, F. (2014). 'Aircraft Automatic Control Systems and their Control Systems', NAŠE MORE, 61(1-2), str. S9-12. Preuzeto s: https://hrcak.srce.hr/121592 (Datum pristupa: 22.01.2021.)
Vancouver Bréda R, Adamčík F. Aircraft Automatic Control Systems and their Control Systems. NAŠE MORE [Internet]. 2014 [pristupljeno 22.01.2021.];61(1-2):S9-12. Dostupno na: https://hrcak.srce.hr/121592
IEEE R. Bréda i F. Adamčík, "Aircraft Automatic Control Systems and their Control Systems", NAŠE MORE, vol.61, br. 1-2, str. S9-12, 2014. [Online]. Dostupno na: https://hrcak.srce.hr/121592. [Citirano: 22.01.2021.]
Sažetak The high reliability of automatic control systems of aircraft is reflected in the practical implementation in order to reduce an already small number of elements, for example, connecting functional element checking and control circuits. Each of the elements of control, which represents a control circuit, also performs the function of the sensor control. It is similar to the element-node connections and can be a wave form that is used for controlling. This is the way how to use converters that perform functions such as comparators from which the output control signal passes to the input power member. The converters, power members, signalling devices and indicators, as well as programming elements are usually placed in the critical nodes and they are elements of not only embedded system checkings, but also backup elements of the aircraft automatic control system.