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Article

A Fast Midcourse Trajectory Optimization Method for Interceptors Based on the Bézier Curve

1
Research Center of Satellite Technology, Harbin Institute of Technology, Harbin 150080, China
2
State Key Laboratory of Micro-Spacecraft Rapid Design and Intelligent Cluster, Harbin 150001, China
*
Author to whom correspondence should be addressed.
Aerospace 2025, 12(10), 893; https://doi.org/10.3390/aerospace12100893
Submission received: 24 July 2025 / Revised: 30 September 2025 / Accepted: 30 September 2025 / Published: 2 October 2025
(This article belongs to the Special Issue Spacecraft Trajectory Design)

Abstract

This paper proposes a fast midcourse trajectory optimization method by using the Bézier curve as a transcription scheme to represent the interceptor trajectories. First, the trajectory optimization problem is established with the constraints during midcourse guidance and the performance index of the terminal velocity. Then, the interceptor position coordinates are represented using Bézier functions, which directly satisfy the boundary constraints. Other state and control variables are also expressed as Bézier functions. Finally, the original trajectory optimization problem is transformed into optimizing the Bézier parameters, which can be obtained by sequential quadratic programming. Numerical examples verify the rapidity of the proposed method when compared with various traditional numerical optimization methods. In addition, the result of the proposed method can be used as a fast solution satisfying all the boundary and path constraints, and it can also be used as an initial guess for further optimizations.
Keywords: Bézier curve; midcourse guidance; trajectory optimization Bézier curve; midcourse guidance; trajectory optimization

Share and Cite

MDPI and ACS Style

Li, J.; Zhang, G.; Cui, L. A Fast Midcourse Trajectory Optimization Method for Interceptors Based on the Bézier Curve. Aerospace 2025, 12, 893. https://doi.org/10.3390/aerospace12100893

AMA Style

Li J, Zhang G, Cui L. A Fast Midcourse Trajectory Optimization Method for Interceptors Based on the Bézier Curve. Aerospace. 2025; 12(10):893. https://doi.org/10.3390/aerospace12100893

Chicago/Turabian Style

Li, Jingqi, Gang Zhang, and Liang Cui. 2025. "A Fast Midcourse Trajectory Optimization Method for Interceptors Based on the Bézier Curve" Aerospace 12, no. 10: 893. https://doi.org/10.3390/aerospace12100893

APA Style

Li, J., Zhang, G., & Cui, L. (2025). A Fast Midcourse Trajectory Optimization Method for Interceptors Based on the Bézier Curve. Aerospace, 12(10), 893. https://doi.org/10.3390/aerospace12100893

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