DERIVATION OF ATTAINABILITY DOMAIN FOR NONLINEAR CONTROLLABLE SYSTEM
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.