Applied Physics and Mathematics Annotation << Back INVESTIGATION OF THE CRITERION FOR THE DEGREE OF OUTPUT CONTROLLABILITY IN THE SYNTHESIS OF A CONTROL SYSTEM FOR A HIGHLY MANEUVERABLE AIRCRAFT WITH ANGULAR ACCELERATION FEEDBACK KHU YUYKHUEY, K.A. NEUSYPIN, M.S. SELEZNEVA, A.V. PROLETARSKIY The problem of synthesis of the control system of a highly maneuverable aircraft (HMA) based on the output of the SIMO system is considered. A new structure of the control system with feedback on angular acceleration is proposed. A new criterion for the degree of controllability of the system output has been developed. A systematic analysis of the characteristics of the proposed control system was carried out in comparison with the feedback on the angular velocity with the developed criterion. The results of numerical simulations with different characteristics of the static stability of AMLA are presented. Keywords: controllability criterion, highly maneuverable aircraft, angular acceleration feedback, static stability. DOI: 10.25791/pfim.06.2022.1244 Pp. 10-16.