Partitioning of centralized integrated flight/propulsion control design for decentralized implementation
作者： S. Garg
DOI: 10.1109/87.238402
关键词:
摘要: The notion of partitioning a centralized controller into decentralized, hierarchical structure suitable for integrated flight/propulsion control (IFPC) implementation is discussed. A systematic procedure developed determining partitioned airframe and engine subsystem controllers (subcontrollers), with the desired interconnection structure, that approximate closed-loop performance robustness characteristics given controller. demonstrated by application to IFPC design short take-off vertical landing (STOVL) aircraft in landing-approach-to-hover-transition flight phase. >
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