A conceptual method for implementation of anytime algorithms for a small turbojet engine

The article presents a method for implementation of "anytime" algorithms into digital real-time control system for a small turbojet engine iSTC-21v. This method presents an approach that will be used for future work in design of the control system. The presented method is an extension of the actual developed control system of engine, which uses the theory of situational control of complex systems. This control system uses progressive control algorithms. For practical implementation of this control system it is important to think about computational complexity. Control systems of aircraft engines use computer (Full Authority Electronic engine control — FADEC) with limited computation resources. Aircraft engines work in environment with stochastic conditions. It is necessary to ensure reliable and stable operation of engine. Anytime algorithms can help to solve this problem and to meet the safety requirements.