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Full Length Article | Open Access

Analytical reentry guidance framework based on swarm intelligence optimization and altitude-energy profile

Hui XUa, Guangbin CAIa( ), Chaoxu MUb, Xin LIa
College of Missile Engineering, Rocket Force University of Engineering, Xi’an 710025, China
School of Electrical and Information Engineering, Tianjin University, Tianjin 300072, China
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Abstract

Aimed at improving the real-time performance of guidance instruction generation, an analytical hypersonic reentry guidance framework is presented. The key steps of the novel guidance framework are the parameterization of reentry guidance problems and the optimization of parameters. First, a quintic polynomial function of energy was designed to describe the altitude profile. Then, according to the altitude-energy profile, the altitude, velocity, flight path angle, and bank angle were obtained analytically, which naturally met the terminal constraints. In addition, the angle of the attack profile was determined using the velocity parameter. The swarm intelligent optimization algorithms were used to optimize the parameters. The path constraints were enforced by the penalty function method. Finally, extensive simulations were carried out in both nominal and dispersed cases, and the simulation results showed that the proposed guidance framework was effective, high-precision, and robust in different scenarios.

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Chinese Journal of Aeronautics
Pages 336-348

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Cite this article:
XU H, CAI G, MU C, et al. Analytical reentry guidance framework based on swarm intelligence optimization and altitude-energy profile. Chinese Journal of Aeronautics, 2023, 36(12): 336-348. https://doi.org/10.1016/j.cja.2023.07.029

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Received: 15 November 2022
Revised: 15 December 2022
Accepted: 02 February 2023
Published: 02 August 2023
© 2023 Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).