AUTOMATIC CONTROL CONTOURS OF UAV USING ONLY RELIABLE INFORMATION FROM SENSORS OF DIRECT MEASUREMENT INFORMATION

M. K. Filyashkin, A. P. Prymak, A. N. Babeniuk

Abstract


This paper presents principles of the reconfiguration of automatic control loops of UAV inwhich at the stage of exit from zone of the active jamming uses only reliable information that's obtainedonly by autonomous measurement and can't cause the loss of the UAV. Designed control laws of the UAV’s autopilot and execute their comprehensive investigation

Keywords


Аngles of roll and pitch; unreliable information; autonomous measurement; control loops; laws aileron and elevator

References


V. M. Sineglazov, M. K. Filyashkin. Automatic control systems of aircraft. Kyiv: Edition NAU, 2004. 502 p. (in Ukrainian)

V. O. Rogozhin, V. M. Sineglazov, M. K. Filyashkin. Flight navigation complexes of aircraft. Kyiv: Edition NAU, 2005. 316 p. (in Ukrainian)

M. P. Mukhina, “Visual slam algorithm using correlation extremal principle”. Electronics and Control Systems, no. 4 (36), 2013. pp. 9–12.


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