Decentralized Design for Integrated Flight/Propulsion Control of Aircraft

摘要: A direct decentralized approach to the design of integrated flight/propulsion control (IFPC) systems is considered in order reduce complexity and validation drawbacks centralized designs. The imposed triangular structure on IFPC controller allows for separate evaluation engine as well achievable performance overall system. Hco techniques which require solution Riccati-like equations are used develop method. This method applied an aircraft aero-propulsive model results indicate that may be a vital alternative other appearing literature. coordinate functions both flight propulsion systems.