Time-Triggered State-Machine Reliable Software Architecture for Micro Turbine engine control

摘要：

Time-Triggered embedded software pattern is well accepted in aerospace industry for its high reliability.Finite-State- Machine 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 25kg thrust micro turbine engine used for UAV system.Experiments results show that Time-Triggered State-Machine software 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 Engine control

作者: ZHANG Qi XU Guoqiang Ding Shuiting

作者单位: School of Transportation Science and Technology,Beihang University,Beijing,China,100191 National Key Laboratory of Science and Technolgy on Aero-engine Aerothermodynamics,Beihang Universit

会议类型: 国际会议

会议名称: 航空器适航技术与管理国际会议 ISAA 2011

会议地点: 北京

会议语种:英文

页码: 587

在线出版日期: 2011-10-01（万方平台首次上网日期，不代表论文的发表时间）