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Алгоритм коррекции навигационного комплекса на основе дифференциального игрового подхода
The problem of a zero-sum differential stabilization game with a quadratic performance functional is considered. The navigation system of an aircraft, including a platform inertial navigation system with structural correction using a control algorithm, is investigated. Errors of the navigation system, subject to the influence of uncontrolled disturbances, are described by a nonlinear ordinary differential equation. It is known that the synthesis of optimal feedback controls leads to the need to solve the scalar Bellman-Isaacs partial differential equation at the pace of system operation. To solve this equation, a method for equivalent transformation of the original nonlinear equation of the plant into a model with a linear structure, but with state-dependent parameters is proposed. This allows one to rewrite the Bellman equation as a Riccati equation with state-dependent parameters. An algorithm for solving this equation is proposed. The performance of the developed algorithm was tested using a flight experiment.