ISSN 0021-3454 (print version)
ISSN 2500-0381 (online version)
Menu

8
Issue
vol 67 / August, 2024
Article
UDC 681.5.01:629.7.05

DERIVATION OF ATTAINABILITY DOMAIN FOR NONLINEAR CONTROLLABLE SYSTEM



Read the full article 

Abstract. The problem of attainability domain derivation for an aircraft is considered. A method is proposed to take into account perturbations of unknown statistical characteristics. The attainability domain is derived point by point on the base of a subsidiary conflict problem solved with the use of proposed iteration algorithm. A program is developed which realizes the method and demonstrates effectiveness of its application.
Keywords: attainability domain, conflict problem, stabilization system, optimal control.