Infrared and Laser Engineering, Volume. 51, Issue 8, 20210956(2022)
Trajectory optimization design of ascending stage of RBCC powered hypersonic vehicle
[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] P Lu, H Sun, B Tsai. Closed-loop endoatmospheric ascent guidance. 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] Huifeng Li, Zhaoying Li. Study on indirect method of optimal guidance in ascending phase of hypersonic vehicle. Acta Astronautica, 32, 297-302(2011).
[5] J Derek, F Driscoll. Minimum-fuel ascent of a hypersonic vehicle using surrogate optimization. Journal of Aircraft, 51, 1973-1986(2014).
[6] Xiaodong Yan, Xiaojuan Jia, Shi Lv. Isobaric climb method for RBCC powered aircraft. 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] Chunlin Gong, Lu Han, Liangxian Gu. Research on trajectory optimization modeling for RBCC carrier. Acta Astronautica, 34, 1592-1598(2013).
[9] Xiang Li, Chang’an Liu, Zejiang Wang, et al. Range optimization and analysis of an aspirated hypersonic missile. Journal of Ordnance Industry, 33, 290-294(2012).
[10] Hongyu Zhou, Xiaogang Wang, Yali Zhao, et al. Intelligent optimization method for ascending trajectory of combined power vehicle. 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] X Liu. Fuel-optimal rocket landing with aerodynamic controls. Journal of Guidance Control & Dynamics, 42, 65-77(2019).
[13] Jiawei Wang, Ran Zhang, Zeming Hao, et al. Real time trajectory optimization of aerospace vehicle based on proximal-Newton-Kantorovich convex programming. 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] Ben Yang, Tianren Li, Xiaoyuan Ma. Fast trajectory optimization with multiple constraints based on sequential convex optimization. Aerospace Control, 38, 25-30(2020).
[16] Aiqiang Guo, Tianpeng Li, Xiaonan Li, et al. Simulation of smoke jamming laser terminal guided projectile. Infrared and Laser Engineering, 51, 20210225(2022).
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Zhe Luo, Shumei Wang, Xunliang Yan, Xinsan Li. Trajectory optimization design of ascending stage of RBCC powered hypersonic vehicle[J]. Infrared and Laser Engineering, 2022, 51(8): 20210956
Category: Image processing
Received: Nov. 30, 2021
Accepted: --
Published Online: Jan. 9, 2023
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