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作 者:ZHANG Qi XU Guoqiang DING Shuiting
机构地区:[1]School of Transportation Science and Technology, Beihang University, Beijing 100191, China [2]National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, Beihang University, Beijing 100191, China
出 处:《Chinese Journal of Aeronautics》2012年第6期839-845,共7页中国航空学报(英文版)
摘 要:Time-triggered (TT) embedded software pattern is well accepted in aerospace industry for its high reliability. Fi-nite-state-machine (FSM) design method is widely used for its high efficiency and predictable behavior. In this paper, the time-triggered and state-machine combination software architecture is implemented for a 25 kg thrust micro turbine engine (MTE) used for unmanned aerial vehicle (UAV) system; also model-based-design development workflow for airworthiness software directive DO-178B is utilized. Experimental results show that time-triggered state-machine software architecture and development method could shorten the system development time, reduce the system test cost and make the turbine engine easily comply with the airworthiness rules.Time-triggered (TT) embedded software pattern is well accepted in aerospace industry for its high reliability. Fi-nite-state-machine (FSM) design method is widely used for its high efficiency and predictable behavior. In this paper, the time-triggered and state-machine combination software architecture is implemented for a 25 kg thrust micro turbine engine (MTE) used for unmanned aerial vehicle (UAV) system; also model-based-design development workflow for airworthiness software directive DO-178B is utilized. Experimental results show that time-triggered state-machine software architecture and development method could shorten the system development time, reduce the system test cost and make the turbine engine easily comply with the airworthiness rules.
关 键 词:airworthiness time-triggered finite-state-machine model-based-design turbine engine control
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