[1] Jianhua Wang, Luhua Liu, Peng Wang. Integrated guidance and control scheme for hypersonic vehicles in dive phase. Acta Aeronautica ET Astronautica Sinica, 38, 207-219(2017).
[2] Bing Chen, Yong Zheng, Zhanglei Chen, et al. A review of celestial navigation system on near space hypersonic vehicle. Acta Aeronautica ET Astronautica Sinica, 41, 32-43(2020).
[3] Can Zhang, Xubin Lin, Dongdong Hu, et al. A review of technology development on foreign hypersonic vehicles. Aerodynamic Missile Journal, 1-5, 15(2019).
[4] Sayler K M. Hypersonic Weapons: Background Issues f Congress[R]. Washington D C: Congressional Research Service, 2019.
[5] Howard A E. Fast furiously accurate[C]Emerging & Disruptive Technologies Essay Contest, 2019.
[6] Ouzt P J, Soloway D I, Moerder D D, et al. The role of guidance, navigation, control in hypersonic vehicle multidisciplinary design optimization[C]16th AIAADLRDGLR International Space Planes & Hypersonic Systems & Technologies Conference, 2009.
[7] Wei Zhang, Heng Zhang. Research on problems of celestial navigation in space engineering. Journal of Deep Space Exploration, 204-213(2016).
[8] Quan Wei, Liu Baiqi, Gong Xiaolin, et al. INSCNSGNSS Integrated Navigation Technology[M]. Beijing: National Defense Industry Press, 2011. (in Chinese)
[9] Zhiping Han, Xingliang Yin. A method to calculate modulation transfer function for aerodynamic optical effect. Modern Defence Technology, 28, 30-35(2000).
[10] Lin Wu, Jiancheng Fang, Zhaohua Yang. Study on aero-optical distortion simulation of high refraction index gradient regions in hypersonic turbulent flow. Acta Optica Sinica, 29, 2952-2957(2009).
[11] Xue Kong, Guodong Ning, Ming Yang, et al. Study on aero optical effect of star navigation imaging. Infrared and Laser Engineering, 47, 1031001(2018).
[12] Yihan Li, Haiyang Hu, Qiang Wang. Radiative transmission property of infrared window in hypersonic vehicle. Infrared and Laser Engineering, 49, 0404002(2020).
[13] K Kourta, R Sauvage. Computation of supersonic mixing layers. Physics of Fluids, 14, 3790-3797(2002).
[14] Jiangfeng Wang, Xudong Wang, Jiawei Li, et al. Overview on aerodynamic design of cruising waverider configuration for hypersonic vehicles. Acta Aerodynamica Sinica, 36, 705-728(2018).
[15] B John, V Kulkarni. Effect of leading edge bluntness on the interaction of ramp induced shock wave with laminar boundary layer at hypersonic speed. Computers & Fluids, 96, 177-190(2014).
[16] Yong Chen, Longde Guo, Long Zhang, et al. Investigation on aero-optical effects of high-speed turbulence over a slope with a cavity. Acta Aerodynamica Sinica, 28, 666-671(2010).
[17] A G Hammitt, S M Bogdonoff. Hypersonic studies of the leading-edge effect on the flow over a flat plate. Journal of Jet Propulsion, 26, 241-246(1956).
[18] Chen Shuxing. Mathematical Analysis of Shock Wave Reflection[M]. Shanghai: Shanghai Scientific & Technical Publishers, 2018: 19. (in Chinese)
[19] J M Kendall. An experimental investigation of leading-edge shock-wave-boundary-layer interaction at Mach 5.8. Journal of the Aeronautical Sciences, 24, 47-56(1957).
[20] R W Garvine. Shock wave transport effects on hypersonic leading edge flow. AIAA Journal, 4, 1856-1858(1966).
[21] T D Butler. Numerical solutions of hypersonic sharp-leading-edge flows. Physics of Fluids, 10, 1205(1967).
[22] Yin Xingliang. Principle of AeroOptics[M]. Beijing: China Aerospace Publishing House, 2003: 169173. (in Chinese)
[23] A A Maslov, S G Mironov, T V Poplavskaya, et al. Stability of hypersonic shock layer on plane plate. Fluid Dynamics, 39, 181-188(2004).
[24] Kun Li, Ping Li, Huimin Chen. Study of refraction and reflection effect caused by shock wave on laser short-range detection. Acta Armamentarii, 29, 28-32(2008).
[25] Liepmann H W, Roshko A. Elements of Gasdynamics[M]. New Yk: Dover Publications, 1956: 8687.
[26] Zhongrong Lu. A new analytical method determining the plane oblique shock angle. Journal of Beijing Institute of Aeronautics and Astronautics, 87-92(1988).
[27] Yan Zhao, Tao Wang, Dong Xu, et al. CFD grids-based transmission model of the rays propagating through the hypersonic flow field. Acta Armamentarii, 29, 282-286(2008).
[28] Williams T, Bolender M A, Doman D B. An aerothermal flexible mode analysis of a hypersonic vehicle[C]Aiaa Atmospheric Flight Mechanics Conference & Exhibit, Keystone, 2006.
[29] Truesdale N, Skeen M, Diller J, et al. DayStar: Modeling the daytime perfmance of a star tracker f high altitude balloons[C]Aiaa Aerospace Sciences Meeting Including the New Hizons Fum & Aerospace Exposition, 2013.
[30] Kan Wang, Meng Wang. On the accuracy of Malley probe measurements of aero-optical effects: a numerical investigation. Optical Engineering, 52, 071407(2013).
