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Research Article

Improved two-phase sequential convex programming for reentry trajectory optimization

Guangbin Cai1( ), Hao Wei1, Hui Xu1, Bin Zhou2, Mingzhe Hou2
College of Missile Engineering, Rocket Force University of Engineering, Xi’an 710025, China
Harbin Institute of Technology, Harbin 150001, China
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Abstract

This paper presents an improved two-phase sequential convex programming (SCP) algorithm for reentry trajectory optimization. The continuous-time optimal control problem is first discretized using the Chebyshev pseudospectral method (CPM). A conformal mapping is introduced to redistribute the Chebyshev–Gauss–Lobatto (CGL) nodes, which effectively mitigates the ill-conditioning of the differentiation matrix and enhances numerical stability. The influence of the trust-region radius on the descent behavior of the penalty function is then analyzed, leading to a two-phase optimization strategy. In phase Ⅰ, line-search is adopted to rapidly obtain a feasible solution, thereby avoiding convergence delays caused by prematurely large penalty coefficients. In phase Ⅱ, the step size is finely tuned using trust-region constraints, ensuring both convergence accuracy and improved robustness. Numerical simulations demonstrate that the proposed algorithm achieves superior performance in terms of convergence speed and solution accuracy, while effectively eliminating the numerical oscillations typically induced by excessive penalty coefficients in conventional penalty methods. The framework provides a reliable and efficient numerical approach for reentry trajectory optimization.

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Astrodynamics
Pages 901-919

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Cite this article:
Cai G, Wei H, Xu H, et al. Improved two-phase sequential convex programming for reentry trajectory optimization. Astrodynamics, 2026, 10(5): 901-919. https://doi.org/10.1007/s42064-026-0316-6

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Received: 06 February 2026
Accepted: 29 April 2026
Published: 10 October 2026
© Tsinghua University Press 2026