Infrared and Laser Engineering, Volume. 51, Issue 8, 20210956(2022)

Trajectory optimization design of ascending stage of RBCC powered hypersonic vehicle

Zhe Luo1, Shumei Wang2, Xunliang Yan2, and Xinsan Li1,2
Author Affiliations
  • 1College of Missile Engineering, Rocket Military Engineering University, Xi’an 710025, China
  • 2Academy of Astronautics, Northwestern Polytechnical University, Xi’an 710072, China
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    References(16)

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

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    [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).

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    [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

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    Paper Information

    Category: Image processing

    Received: Nov. 30, 2021

    Accepted: --

    Published Online: Jan. 9, 2023

    The Author Email:

    DOI:10.3788/IRLA20210956

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