| [1] 林军. 分布式的光纤光栅反射信号的解调研究[D]. 武汉: 武汉理工大学, 2008: 72.[2] Wang Y, Gong J, Wang D Y, et al. A quasi-distributed sensing network with time-divisionmultiplexed fiber Bragg gratings [J]. IEEE Photonics Technology Letters, 2011, 23(2): 70-72.[3] Wang W, Gong J, Dong B, et al. A large serial time-division multiplexed fiber Bragg grating sensor network [J]. Journal of Lightwave Technology, 2012, 30(17): 2751-2756.[4] Rogers A. Distributed optical-fibre sensing [J]. Measurement Science and Technology, 1999, 10(8): 75-99.[5] Davis M A, Kersey A D. Simultaneous measurement of temperature and strain using fibre Bragg gratings and Brillouin scattering [J]. Optoelectronics, IEE Proceedings-IET, 1997, 144(3): 151-155.[6] Rogers A J, Shatalin S V, Kanellopoulos S E. Distributed measurement using optical fibre backscatter polarimetry [C]//Optical Fibre Sensors Conference Technical Digest. 2004: 367-370.[7] Froggatt M, Soller B, Gifford D, et al. Correlation and keying of Rayleigh scatter for loss and temperature sensing in parallel optical networks [C]//Optical Fiber Communication Conference. 2004: 1-3.[8] Frovel M, Del O E, Fernandez A, et al. Damage detection by load path changes in reinforced composite panels using local FBGs and distributed sensing [J]. The Prognostics and Health Management (PHM) Society, 2012, 7(2): 1-8.[9] 杨波, 彭俊毅. 光纤光栅传感器在现代大型飞机中的应用探讨[C]// 大型飞机关键技术高层论坛暨中国航空学会2007 年学术年会. 2007: 531-535.[10] 姜德生, 何伟. 光纤光栅传感器的应用概况[J]. 光电子·激光, 2002, 13(4): 420-430.[11] 常飞, 韩庆, 尚柏林. 光纤技术在军用飞机结构健康监控中的研究[J]. 科学技术与工程, 2008, 8(10): 2641-2646.[12] Lee J R, Ryu C Y, Koo B Y, et al. In-flight health monitoring of a subscale wing using a fiber Bragg grating sensor system [J]. Smart Materials and Structures, 2003, 12(1): 147-155.[13] Elster J L, Trego A, Catterall C, et al. Flight demonstration of fiber optic sensors [C]// Smart Structures and Materials 2003: Smart Sensor Technology and Measurement Systems. 2003: 34-42.[14] 薛景锋, 宋昊, 王文娟. 光纤光栅在航空结构健康监测中的应用前景[J]. 航空制造技术, 2012, 22: 45-49.[15] Trutzel M N, Wauer K, Betz D, et al. Smart sensing of aviation structures with fiber optic Bragg grating sensors [C]// Smart Structures and Materials 2000: Sensory Phenomena andMeasurement Instrumentation for Smart Structures and Materials. 2000: 134-143.[16] Betz D, Staudigel L, Trutzel M N. Test of a fiber Bragg grating sensor network for commercial aircraft structures [C]// IEEE 15th Optical Fiber Sensors Conference Technical Digest.2002: 55-58.[17] Fernandez-Lopez A, Menendez J M, Guemes A. Damage detection in a stiffened curved plate by measuring differential strains [C]//16th International Conference on Composite Materials. 2007: 1-8.[18] Ogisu T, Shimanuki M, Kiyoshima S, et al. Development of damage monitoring system for aircraft structure using a PZT actuator/FBG sensor hybrid system [C]//Smart Structures and Materials 2004: Industrial and Commercial Applications of Smart Structures Technologies. 2004: 425-436.[19] Aoki T, Yokozeki T. Some of the topics in composites research projects in Japan [C]// 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.2009: 1-20.[20] Kressel I, Botsev Y, Leibovich H, et al. Fiber Bragg grating sensing in smart composite patch repairs for aging aircraft [C]// 17th International Conference on Optical Fibre Sensors.2005: 1040-1043.[21] Konrath R, Schlager B, Kirmse T, et al. Simultaneous measurements of unsteady aerodynamic loads, flow velocity fields, position and wing deformations of MAVs in plunging motion [M]. Berlin: Springer, 2010: 331-338.[22] 齐共金, 雷洪, 景鹏, 等. 基于先进传感器技术的航空材料无损检测进展[J].航空制造技术, 2009(4): 51-53.[23] 芦吉云. 光纤智能夹层自诊断系统研究[D]. 南京: 南京航空航天大学, 2006: 78.[24] Schweikhard K A, Richards W L, Theisen J, et al. Flight demonstration of X-33 vehicle health management system components on the F/A-18 systems research aircraft [R]. Washington: NASA, 2001.[25] Hess A, Fila L. The joint strike fighter (JSF) PHM concept: potential impact on aging aircraft problems [C]// IEEE Aerospace Conference Proceedings. 2002: 3021-3026.[26] Ecke W, Latka I, Willsch R, et al. Optical fiber grating strain sensor network for X-38 spacecraft health monitoring [C]// Proceedings of SPIE. 2000: 888-891.[27] 宋昊, 张力, 李欣, 等. 光纤布拉格光栅传感技术及其在航空航天中的应用[C]// 国防科技工业试验与测试技术高层论坛. 2007: 257-263.[28] Mitschke F. Fiber-optic sensors [M]. Berlin: Springer, 2010: 247-256.[29] Ferdinand P, Magne S, Dewynter-Marty V, et al. Applications of Bragg grating sensors in Europe [C]// Optical Fiber Sensors. 1997: 14-19.[30] Kressel I, Handelman A, Botsev Y, et al. Evaluation of flight data from an airworthy structural health monitoring system integrally embedded in an unmanned air vehicle [C]// 6thEuropean Workshop on Structural Health Monitoring. 2012: 193-200.[31] Garbos R, Mouyos W. X-33/RLV: system health management/vehicle health management [C]// 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference and Adaptive Structures Forum. 1998: 1857-1864.[32] Wieslaw S, Boller C, Tomlinson G R, et al. Health monitoring of aerospace structures: smart sensor technologies and signal processing [M]. Hoboken, NJ: John Wiley and Sons, 2004.[33] 袁慎芳,邱雷,吴建, 等. 大型飞机的发展对结构健康监测的需求与挑战[J].航空制造技术, 2009, 22: 62-67.[34] Ecke W, Grimm S, Latka I, et al. Optical fiber grating sensor network based on highly reliable fibers and component for spacecraft health monitoring [C]// SPIE’s 8th Annual International Symposium on Smart Structures and Materials. 2001: 160-167.[35] 芦吉云, 梁大开, 潘晓文. 基于准分布式光纤光栅传感器的机翼盒段载荷监测[J]. 南京航空航天大学学报, 2009, 41(2): 218-221.[36] 杜善义, 张晓晶, 陈吉安, 等. 光纤氢传感技术的研究现状及其应用前景[J]. 宇航学报, 2004, 25(4): 466-472.[37] 杜善义, 张博明. 飞行器结构智能化研究及其发展趋势[J]. 宇航学报, 2007, 28(4): 773-778. |
