COMPLEMENTARY FILTER IN INERTIAL-DOPPLER SYSTEM OF NAVIGATION.

Autor: Filyashkin, M. K., Kemenyash, Yu. M.

Publikováno v: Electronics & Control Systems; 2024, Vol. 80 Issue 2, p94-99, 6p

AIRCRAFT FUEL MEASUREMENT SYSTEM BASED ON HYDROSTATIC PRESSURE SENSORS.

Autor: Smirnov, O. I., Filyashkin, M. K.

Publikováno v: Electronics & Control Systems; 2023, Vol. 77 Issue 3, p77-82, 6p

COMPUTER MODELING OF ACCURACY CHARACTERISTICS OF STRAPDOWN INERTIAL NAVIGATION SYSTEM

Autor: Mukhina, M. P., Filyashkin, M. K.

Publikováno v: Radio Electronics, Computer Science, Control; № 4 (2019): Radio Electronics, Computer Science, Control; 157-165
Радиоэлектроника, информатика, управление; № 4 (2019): Радиоэлектроника, информатика, управление; 157-165
Радіоелектроніка, iнформатика, управління; № 4 (2019): Радіоелектроніка, інформатика, управління; 157-165

Context. The problem of correction for operation of strapdown inertial navigation system used for unmanned aerial vehicle is urgent because of further increased requirements to autonomous flight in blackout zones. The object of the study was to simul

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=scientific_p::00d5b3a606c01ed4fff618bf465a1f99
http://ric.zntu.edu.ua/article/view/193677

SHORT RUNWAY LANDING AUTOMATION. (English)

Autor: Filyashkin, M. K., Sidorenko, M. V.

Publikováno v: Electronics & Control Systems; 2020, Vol. 64 Issue 4, p51-56, 6p

COMPENSATION OF QUADRATURED ERROR IN THE AUTO-OSCILLATION MICROMECHANICAL GYROSCOPE.

Autor: Filyashkin, M. K., Chernyay, O. I.

Publikováno v: Electronics & Control Systems; 2018, Vol. 4 Issue 58, p95-100, 6p