Aerospace Instrument-Making Annotation << Back SPECIFICS OF AIRCRAFT WHEEL BRAKING CONTROL SYSTEM IMPLEMENTATION Yu.G. Ionov, L.V. Makolkin Key problems of aircraft landing run and braking in uncertain conditions were described. Using modern control theory an automated control system of aircraft wheel braking was developed. The system based on an adaptive optimal self-organized regulator with extrapolation. Also, a mockup of digital wheel braking unit was created and its specification and features were presented in this article. Key words: aircraft, landing, braking, control, antiskid, software debugging, Matlab. Contacts: E-mail: mleonidos@gmail.com Pp. 03-10.