{"title":"A service availability simulation for the ATDRSS space segment","authors":"J. Broderick, R. Bruno, A. Weinberg","doi":"10.1109/MILCOM.1988.13514","DOIUrl":null,"url":null,"abstract":"A Monte Carlo service availability simulation (SAS) model has been developed as a tool to support the architecture evaluation process for NASA's Advanced Tracking and Data Relay Satellite System (ATDRSS). The key component of the simulation is the spacecraft (S/C) reliability model which utilizes data on S/C subsystems for component configuration, reliability, and redundancy for the faithful generation of random S/C failures. The SAS logic responds to these failures to simulate the appropriate NASA responses for the launch and deployment of new S/C. The outputs of the simulation include the probability that the system meets projected communications requirements over time, required space-ground link capacity, statistics of future S/C launch dates, and number of S/C required over the system life cycle. The SAS is capable of modeling a broad set of system architectures and S/C configurations. Sample applications are described.<<ETX>>","PeriodicalId":66166,"journal":{"name":"军事通信技术","volume":"27 1","pages":"1021-1025 vol.3"},"PeriodicalIF":0.0000,"publicationDate":"1988-10-23","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"军事通信技术","FirstCategoryId":"1093","ListUrlMain":"https://doi.org/10.1109/MILCOM.1988.13514","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 1
Abstract
A Monte Carlo service availability simulation (SAS) model has been developed as a tool to support the architecture evaluation process for NASA's Advanced Tracking and Data Relay Satellite System (ATDRSS). The key component of the simulation is the spacecraft (S/C) reliability model which utilizes data on S/C subsystems for component configuration, reliability, and redundancy for the faithful generation of random S/C failures. The SAS logic responds to these failures to simulate the appropriate NASA responses for the launch and deployment of new S/C. The outputs of the simulation include the probability that the system meets projected communications requirements over time, required space-ground link capacity, statistics of future S/C launch dates, and number of S/C required over the system life cycle. The SAS is capable of modeling a broad set of system architectures and S/C configurations. Sample applications are described.<>