[1] [1] Gong C, Chen B, Gu L. Design optimization of RBCC powered subbital reusable launch vehicle[C]AIAA International Space Planes & Hypersonic Systems & Technologies Conference, 2013.

[2] Lu P, Sun H, Tsai B. Closed-loop endoatmospheric ascent guidance[J]. Journal of Guidance, Control, & Dynamics, 26, 283-294(2003).

[3] [3] Pan B, Lu P. Improvements to optimal launch ent guidance[C]Aiaa Guidance, Navigation, & Control Conference, 2010.

[4] Li Huifeng, Li Zhaoying. Study on indirect method of optimal guidance in ascending phase of hypersonic vehicle[J]. Acta Astronautica, 32, 297-302(2011).

[5] Derek J, Driscoll F. Minimum-fuel ascent of a hypersonic vehicle using surrogate optimization[J]. Journal of Aircraft, 51, 1973-1986(2014).

[6] Yan Xiaodong, Jia Xiaojuan, Lv Shi. Isobaric climb method for RBCC powered aircraft[J]. Solid Rocket Technology, 36, 711-714(2013).

[7] [7] Sun Peihua. Climb trajecty design optimization of hypersonic vehicle under control constraints [D]. Nanjing: Nanjing University of Aeronautics Astronautics, 2017. (in Chinese)

[8] Gong Chunlin, Han Lu, Gu Liangxian. Research on trajectory optimization modeling for RBCC carrier[J]. Acta Astronautica, 34, 1592-1598(2013).

[9] Li Xiang, Liu Chang’an, Wang Zejiang, et al. Range optimization and analysis of an aspirated hypersonic missile[J]. Journal of Ordnance Industry, 33, 290-294(2012).

[10] Zhou Hongyu, Wang Xiaogang, Zhao Yali, et al. Intelligent optimization method for ascending trajectory of combined power vehicle[J]. Acta Astronautica, 41, 61-70(2020).

[11] [11] Szmuk M, Acikmese B, Berning A W. Successive convexification f fueloptimal powered ling with aerodynamic drag nonconvex constraints[C]AIAA Guidance, Navigation, & Control Conference, 2015.

[12] Liu X. Fuel-optimal rocket landing with aerodynamic controls[J]. Journal of Guidance Control & Dynamics, 42, 65-77(2019).

[13] Wang Jiawei, Zhang Ran, Hao Zeming, et al. Real time trajectory optimization of aerospace vehicle based on proximal-Newton-Kantorovich convex programming[J]. Journal of Aeronautics, 41, 121-130(2020).

[14] [14] Liu Peijin. Study on modal perfmance influencing facts of RBCC eject rocket [D]. Xi''an: Nthwest University of Technology, 2001. (in Chinese)

[15] Yang Ben, Li Tianren, Ma Xiaoyuan. Fast trajectory optimization with multiple constraints based on sequential convex optimization[J]. Aerospace Control, 38, 25-30(2020).

[16] Guo Aiqiang, Li Tianpeng, Li Xiaonan, et al. Simulation of smoke jamming laser terminal guided projectile[J]. Infrared and Laser Engineering, 51, 20210225(2022).