作者: M Yasar , A Ray , J F Horn
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摘要: AbstractIntegration of flight and propulsion control systems in advanced aircraft has attracted much attention because ever increasing demand on enhancement performance reliability. As the underlying dynamic couplings non-linear interactions are too complex for realtime execution onboard computational platforms, hierarchical hybrid (i.e. combined continuously varying discrete event) architecture is proposed development future generation that will take advantage these mission enhancement. Although original structures retained, event supervisory (DES) would facilitate decision-making operation. DES decisions regarding influence reliability entire vehicle system due to at level dynamics. A two-level...