Spacecraft Reliability And Multi-State Failures - A Statistical Approach
商品資訊
ISBN13：9780470687918
出版社：John Wiley & Sons Inc
作者：Saleh
出版日：2011/03/18
裝訂／頁數：精裝／216頁
規格：24.1cm*16.5cm*1.9cm (高/寬/厚)
商品簡介
The authors provide new results pertaining to spacecraft reliability based on extensive statistical analysis of on-orbit anomaly and failure data that will be particularly useful to spacecraft manufacturers and designers, for example in guiding satellite (and subsystem) test and screening programs and providing an empirical basis for subsystem redundancy and reliability growth plans. The authors develop nonparametric results and parametric models of spacecraft and spacecraft subsystem reliability and multi-state failures, quantify the relative contribution of each subsystem to the failure of the satellites thus identifying the subsystems that drive spacecraft unreliability, and propose advanced stochastic modeling and analysis tools for the reliability and survivability of spacecraft and space-based networks.
Spacecraft Reliability and Multi-state Failures
- provides new nonparametric results pertaining to spacecraft reliability based on extensive statistical analysis of on-orbit anomaly and failure data;
- develops parametric models of spacecraft and spacecraft subsystem reliability and multi-state failures
- quantifies the relative contribution of each subsystem to the failure of the satellites
- proposes advanced stochastic modeling and analysis tools for the reliability and survivability of spacecraft and space-based networks.
- provides a dedicated treatment of the reliability and subsystem anomalies of communication spacecraft in geostationary orbit.
作者簡介
Joseph Homer Saleh, Georgia Institute of Technology
Joe Saleh joined Georgia Institute of Technology as Assistant Professor of Aerospace Engineering in 2007, having previous served as the Executive Director of the Ford-MIT Alliance. He is an Associate Fellow of the American Institute of Aeronautics and Astronautics (AIAA), and in 2008 won the Most Valuable Professor (MVP) award, School of Aerospace Engineering, Georgia Institute of Technology. He has authored two books, Analyses for Durability and System Design Lifetime: A Multidisciplinary Approach (2008) and Reliability and Risk Analysis: A Friendly Introduction (forthcoming), as well as circa 40 journal papers and 50 conference papers.
Jean-Francois Castet is a student at Georgia Institute of Technology. He is working on developing a framework for characterizing and analysing survivability and resiliency of spacecraft and space-based networks. Some parts of his research also focus on updating satellite reliability models.
目次
1.1 On time and reliability.
1.2 On spacecraft and reliability: early studies.
1.3 Book organization.
2 Nonparametric reliability analysis of spacecraft failure data.
2.1 Introduction.
2.2 Database and data description.
2.3 Nonparametric analysis of spacecraft failure data.
2.4 Confidence interval analysis.
2.5 Discussion and limitation.
2.A Appendix.
3 Parametric analysis and Weibull modeling of spacecraft reliability.
3.1 Weibull distribution: an overview.
3.2 Probability plots or graphical estimation.
3.3 Maximum likelihood estimation (MLE).
3.4 Comparative analysis of the spacecraft reliability parametric fits.
3.5 Finite mixture distributions.
3.6 Comparative analysis of the single versus the mixture distribution Weibull fits.
4 Data specialization: statistical analysis of spacecraft reliability by orbit and mass categories.
4.1 Introduction.
4.2 Data description and mass categorization.
4.3 Nonparametric analysis of satellite reliability by mass category.
4.4 Parametric analysis of satellite reliability by mass category.
4.5 Orbit characterization.
4.6 Nonparametric analysis of spacecraft reliability by mass and orbit category.
4.7 Parametric analysis of satellite reliability by mass and orbit category.
4.8 Hypotheses for causal explanations.
4.A Appendix: Tabular data and confidence interval analysis.
5 Spacecraft subsystem reliability.
5.1 Spacecraft subsystem identification.
5.2 Nonparametric reliability analysis of spacecraft subsystems.
5.3 Weibull modeling of spacecraft subsystem reliability.
5.4 Comparative analysis of subsystem failures.
6 Time to anomaly and failure of spacecraft subsystems: exploratory data analysis.
6.1 Introduction.
6.2 Anomaly and failure events.
6.3 Distribution of anomalies and failure events by subsystem.
6.4 Time to anomaly and failure of spacecraft subsystems.
7 Multi-state failure analysis of spacecraft subsystems.
7.1 Introduction.
7.2 Setting the stage: multi-state failure analysis and the state transition diagram.
7.3 Nonparametric analyses of spacecraft subsystems' multi-state failures.
7.4 Parametric analyses of spacecraft subsystems' multi-state failures.
7.5 Comparative reliability and multi-state failure analysis of spacecraft subsystems.
7.A Appendix.
8 Toward survivability analysis of spacecraft and space-based networks.
8.1 Introduction.
8.2 Overview of survivability and resiliency.
8.3 Survivability framework.
8.4 Introduction to SPNs.
8.5 SPNs for spacecraft modeling and survivability analysis.
8.A Appendix: SPN model of the SBN in Figure 8.6 and its schematic explanation.
Epilogue.
Appendix A Geosynchronous communication. satellites: system reliability and subsystem anomalies and failures.
A.1 Part I: System reliability analysis.
A.2 Part II: Subsystem anomalies and failures.
Appendix B Electrical power subsystem: comparative analysis of failure events in LEO and GEO.
B.1 Introduction.
B.2 Database, sample analyzed, and classes of failure events.
B.3 Brief literature review.
B.4 Reliability and multi-state failure analyses of the EPS.
B.5 Comparative analysis of the EPS failure in LEO and GEO.
B.6 Conclusion.
References.
Index.
購物須知
外文書商品之書封，為出版社提供之樣本。實際出貨商品，以出版社所提供之現有版本為主。部份書籍，因出版社供應狀況特殊，匯率將依實際狀況做調整。
無庫存之商品，在您完成訂單程序之後，將以空運的方式為你下單調貨。為了縮短等待的時間，建議您將外文書與其他商品分開下單，以獲得最快的取貨速度，平均調貨時間為1~2個月。
為了保護您的權益，「三民網路書店」提供會員七日商品鑑賞期(收到商品為起始日)。
若要辦理退貨，請在商品鑑賞期內寄回，且商品必須是全新狀態與完整包裝(商品、附件、發票、隨貨贈品等)否則恕不接受退貨。