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报告编号NASA-CR-174168, NAS 1.26:174168
来源IDNTRS_Document_ID: 19850005169
A unified method for evaluating real-time computer controllers: A case study. [aircraft control]
Shin, K. G.; Krishna, C. M.; Lee, Y. H.
英文摘要A real time control system consists of a synergistic pair, that is, a controlled process and a controller computer. Performance measures for real time controller computers are defined on the basis of the nature of this synergistic pair. A case study of a typical critical controlled process is presented in the context of new performance measures that express the performance of both controlled processes and real time controllers (taken as a unit) on the basis of a single variable: controller response time. Controller response time is a function of current system state, system failure rate, electrical and/or magnetic interference, etc., and is therefore a random variable. Control overhead is expressed as a monotonically nondecreasing function of the response time and the system suffers catastrophic failure, or dynamic failure, if the response time for a control task exceeds the corresponding system hard deadline, if any. A rigorous probabilistic approach is used to estimate the performance measures. The controlled process chosen for study is an aircraft in the final stages of descent, just prior to landing. First, the performance measures for the controller are presented. Secondly, control algorithms for solving the landing problem are discussed and finally the impact of the performance measures on the problem is analyzed.
英文关键词AIRCRAFT CONTROL COMPUTER SYSTEMS PERFORMANCE CONTROLLERS FLIGHT CONTROL NUMERICAL CONTROL REAL TIME OPERATION AIRCRAFT LANDING MULTIPROCESSING (COMPUTERS) PERFORMANCE PREDICTION RESPONSE TIME (COMPUTERS)
出版年1982
报告类型Technical Report
语种英语
国家美国
URLhttp://hdl.handle.net/2060/19850005169
资源类型科技报告
条目标识符http://119.78.100.177/qdio/handle/2XILL650/258908
推荐引用方式
GB/T 7714
Shin, K. G.,Krishna, C. M.,Lee, Y. H.. A unified method for evaluating real-time computer controllers: A case study. [aircraft control],1982.
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