Proletarskii

The authors present an original concept of synthesis of intelligent systems controlling dynamic objects; the concept is based on the theory of functional systems formulated by P.K. Anokhin. The authors propose an approach to synthesis of aircraft control systems, using intelligent technologies. In this article different types of intellectualized aircraft control systems are considered.  The authors investigated the most promising intellectualised management system with the acceptor of action which includes genetic algorithms. The authors propose structures of intellectualized control systems for advanced aircraft and consider a method for reducing computational cost for implementation of the genetic algorithm based on application of the procedure of crossing - meiosis.

The article considers methods of identification of center-of-mass motion models in space rockets. Reducing the task of identification to a two-point boundary-value problem is shown for the purpose of unification of program-algorithmic support in the control system.

The problem of aircraft movement control with required accuracy at different segments of flight is usually solved with the usage of information from measurement system. The best structure of a measurement system was determined with the calculation and analysis of precision characteristics of measurement systems.