Optimal Selection Method for Terminal-Guidance Parameters with Complex Constraints Based on the TLBO Algorithm

Simultaneously satisfying multiple constraints while maintaining a relatively simple guidance law remains challenging in terminal guidance. This paper proposes a parameter optimization method based on teaching–learning-based optimization (TLBO). Taking proportional navigation as an example, a bias term is designed to achieve a desired impact angle and two bias term adjustment coefficients are introduced as additional optimization variables to satisfy the seeker blind-zone constraint. The lead-angle and normal acceleration rate constraints are converted into normal acceleration magnitude constraints. With impact time and impact speed as optimization objectives, TLBO is employed to optimize the initial conditions and guidance parameters. Numerical simulations demonstrate the feasibility of the proposed method, and the Monte Carlo results show that satisfactory terminal guidance performance is maintained under the specified normal-acceleration perturbations.

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Publication Details

Journal
Eng—Advances in Engineering
Published
2026-11-03
DOI
https://doi.org/10.3390/eng7110602
Primary Topic
Guidance and Control Systems
Type
article
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article

Optimal Selection Method for Terminal-Guidance Parameters with Complex Constraints Based on the TLBO Algorithm

Shuo Song, Lu Wang, Jiwei Chen, Li Li et al.
Eng—Advances in Engineering
Guidance and Control Systems
article

Optimal Selection Method for Terminal-Guidance Parameters with Complex Constraints Based on the TLBO Algorithm

Shuo Song, Lu Wang, Jiwei Chen, Li Li, Xiaorong Shi
article en

Abstract

Simultaneously satisfying multiple constraints while maintaining a relatively simple guidance law remains challenging in terminal guidance. This paper proposes a parameter optimization method based on teaching–learning-based optimization (TLBO). Taking proportional navigation as an example, a bias term is designed to achieve a desired impact angle and two bias term adjustment coefficients are introduced as additional optimization variables to satisfy the seeker blind-zone constraint. The lead-angle and normal acceleration rate constraints are converted into normal acceleration magnitude constraints. With impact time and impact speed as optimization objectives, TLBO is employed to optimize the initial conditions and guidance parameters. Numerical simulations demonstrate the feasibility of the proposed method, and the Monte Carlo results show that satisfactory terminal guidance performance is maintained under the specified normal-acceleration perturbations.

Eng—Advances in EngineeringVol. 7(11)
Harbin Institute of Technology (CN)
Openalex Percentile: Top 20%
Guidance and Control Systems
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Optimal Selection Method for Terminal-Guidance Parameters with Complex Constraints Based on the TLBO Algorithm — Shuo Song, Lu Wang, et al. · Eng—Advances in Engineering (2026) | TGRS Research Map | TGRS