[1] Boeing. 787 GoldCare-airplane business solutions [EB/OL]. [2011-10-01]. http://www.boeing.com/commercial/goldcare/index.
[2] Zeng S K, Pecht M G, Wu J. The development of prognostic and health management (PHM). Aviation Transaction, 2005, 26(5): 626-633.
[3] Vachtsevanos G, Lewis F, Roemer M, et al. Intelligent fault diagnosis and prognosis for engineering systems. John Wiley & Sons Inc, 2006.
[4] Khalak A, Tierno J. Influence of prognostic health management on logistic supply chain. IProceedings of the 2006 American Control Conference, 2006.
[5] Boller C, Chang F K, Fujino Y. Encyclopedia of structural health monitoring. John Wiley & Sons Inc, 2009.
[6] Propes, Lee S, et al. A real-time architecture for prognostic enhancements to diagnostic systems. Knoxville Proceeding of Marcon 2002 Conference, 2002.
[7] Maier M W, Rechtin E. The art of systems architecting. CRC Press, 2002.
[8] Marbach P R. Directed energy weapon system architecture to meet network centric operations requirements. The 16th Annual International Symposium Proceedings, 2006.
[9] Hempstead M, Tripathi N, Mauro P, et al. An ultra low power system architecture for sensor network applications. 32nd International Symposium on Computer Architecture, 2005.
[10] Ames Research Center NASA. Ames Technology Capabilities and Facilities. Design principles for robust ISHM[EB/OL]. [2008-08-05] http://www.nasa.gov/centers/ames/research/technology-onepagers/ design_principles.html.
[11] Schrage, DeLaurentis D, Taggart K. FCS study: IPPD concept development process for future combat systems. AIAA MDO Specialists Meeting, 2002.
[12] Sullivan P. Quality function deployment. Quality Progress, 1986, 19(6): 39-50.
[13] Montgomery C. Experimental design for product and process design and development. Journal of the Royal Statistical Society, 1999, 48(2):159-177.
[14] Menzies T, Pecheur C. Verification and validation and artificial intelligence. Advances in Computers, 2005(65): 153-201.
[15] He H B, Zhao J M, Xu C A. Cost-benefit model for PHM. Procedia Environmental Sciences, 2011(10): 759-764.
[16] Kessler S S, Amaratunga K S, Wardle B L. An assessment of durability requirements for aircraft structural health monitoring sensors. Proceedings of the 5th International Workshop on Structural Health Monitoring, 2005.
[17] Orsagh F, Roemer M J. Development of metrics for mechanical diagnostic technique qualification and validation. COMADEM Conference, 2000.
[18] RTCA SC167, RTCA/DO-178B: Software Considerations in Airborne Systems and Equipment Certification[S], 1992.
[19] RTCA DO-254: Design Assurance Guidance for Airborne Electronic Hardware[S], 2000.
[20] Department of Defense, MIL-HDBK-516B Handbook: Airworthiness Certification Criteria[S], 2008.
[21] Aviation Engineering Directorate, ADS-79-HDBK: Aeronautical Design Standard Handbook for Condition Based Maintenance Systems for US Army Aircraft[S], 2009.
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