[2] FIORENTINI L,SERRANI A.Adaptive restricted trajectory tracking for a non-minimum phase hypersonic vehicle model［J］.Automatica,2012,48(7):1248-1261.

[7] TRENDAFILOVA I,CARTMELL M P,OSTACHOWICZ W.Vibration-based damage detection in an aircraft wing scaled model using principal component analysis and pattern recognition［J］.Journal of Sound and Vibration,2008,313(3):560-566.

[11] CAPLIN J,RAY A,JOSHI S M.Damage-mitigating control of aircraft for enhanced structural durability［J］.IEEE Transactions on Aerospace and Electronic Systems,2001,37(3):849-862.

[14] GLASS D E.Ceramic Matrix Composite (CMC) Thermal Protection Systems (TPS) and hot structures for hypersonic vehicles［C］//The 15th AIAA Space Planes and Hypersonic Systems and Technologies Conference,2008:1-36.

[15] Haynes International.Haynes230 alloy brochure:No.H-3000［EB/OL］.(2010-08-26)［2016-07-26］.http://haynesintl.com/docs/default-source/pdfs/new-alloy-brochures/high-temperature-alloys/brochures.