[1] WALKER S, SHERK J, SHELL D, et al. The DARPA/AF falcon program: the hypersonic technology vehicle #2(HTV-2) flight demonstration phase[C]//AIAA International Space Planes and Hypersonic Systems and Technologies Conference. Washington DC, USA: American Institute of Aeronautics and Astronautics, 2008: 2539.
[2] WANG L D, ZENG Y H, GAO L, et al. Technology status and development trend for radar detection of hypersonic target in near space[J]. Journal of Signal Processing, 2013, 30(1):73-81(in Chinese).
[3] GU B Y, LI B, LIU R F. Research progress on target characteristics of hypersonic aircraft in foreign countries.Aerodynamic Missile Journal, 2014(5):72-76(in Chinese).
[4] BLANCHARD R, ANDERSON B, WELCH S, et al. Shuttle orbiter fuselage global temperature measurements from infrared images at hypersonic speeds[C]//AIAA Atmospheric Flight Mechanics Conference and Exhibit. Washington DC, USA: American Institute of Aeronautics and Astronautics, 2002: 4702.
[5] BEIER K. Infrared radiation model for aircraft and reentry vehicle[J]. Proceedings of the SPIE, 1988, 972:363-374. doi: 10.1117/12.948320
[6] MAHULIKAR S P, SONAWANE H R, RAO G A. Infrared signature studies of aerospace vehicles[J]. Progress in Aerospace Sciences, 2007, 43(7):218-245.
[7] WU L M, ZHOU F, WANG H Y. Study on the relationship between the infrared detectors background limit detectivity and the optical systems work temperature[J]. Spacecraft Recovery & Remote Sensing, 2010, 31(1):36-41(in Chinese).
[8] WU L M, ZHOU F, WANG H Y. Research of operation range model for detecting moving point target in deep space background.Spacecraft Recovery & Remote Sensing, 2010, 31(3):21-26(in Chinese).
[9] WANG R, HAO X J, ZHOU H Ch, et al. Design of infrared signal detection circuit in a temperature calibration system[J]. Laser Technology, 2013, 37(2):247-250(in Chinese).
[10] WANG Y F, CHEN J. Infrared radiation signature of hypersonic vehicle and its infrared detection and early warning[J]. Tactical Missile Technology, 2011(2):55-57(in Chinese).
[11] ZHOU J W, LI J Ch, SHI Zh G. et al. Research of infrared detectability of hypersonic vehicle[J]. Acta Optica Sinica, 2015, 35(5):0504001(in Chinese). doi: 10.3788/AOS
[12] YANG H, ZHANG Y Sh, DING W Zh. Detectability of airship infrared detection system to hypersonic vehicle[J]. Chinese Optics, 2016, 9(5):596-605(in Chinese). doi: 10.3788/co.
[13] YANG X, NIU Q L, HE Zh H, et al. Analysis of infrared characteristics and detectability of HTV-2 type vehicle[J]. Acta Optica Sinica, 2017, 37(12):1204001(in Chinese).
[14] GLASS D, DIRLING R, CROOP H, et al. Materials development for hypersonic flight vehicles[C]//14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference. Washington DC, USA: American Institute of Aeronautics and Astronautics, 2006: 8122.
[15] XU G X. Optical characteristics of object and environment[M]. Beijing:Astronautic Publishing House, 1995:11-12(in Chinese).
[16] TIAN B, XIE F, FAN Ch Y, et al. Study of detection capability of low orbit infrared detection satellite to high dynamic target in atmosphere[J]. Infrared(Monthly), 2015, 36(5):1-15(in Chinese).
[17] YE Q, SUN X Q, SHAO L. Analysis of optimum detective wavebands for infrared early-warning satellite[J]. Infrared and Laser Engineering, 2010, 39(3):389-393(in Chinese).
[18] LIU Z Y, SHAO L, WANG Y F. et al. A band selection method for infrared warning satellites based on radiation flux apparent contrast spectrum[J]. Journal of Infrared and Millimeter Waves, 2014, 33(5):492-497(in Chinese).
[19] WANG Ch, LI Y, LI J L. et al. Research summary of IR characteristic and contrast between object and background[J]. Ship Electronic Engineering, 2012, 32(1):4-6(in Chinese).