Quantitative Study on the Effective Shielding Time Window of UAV Smoke Grenades Based on Geometric Determination and Kinematic Comparison

Authors

  • Tao Zhao
  • Yifan Chen
  • Jiaqi Liao

DOI:

https://doi.org/10.54097/38hmzb73

Keywords:

Geometric determination, Numerical integration, Smoke shielding quantification

Abstract

This study aims to quantify the effective duration of concealment provided by a single smoke grenade against an incoming missile, thereby optimizing the deployment strategy for drone smoke decoy grenades. Following a problem decomposition—model construction—precise solution framework, this work employs kinematic modeling and geometric detection. Within a unified coordinate system, it extracts the shielding time window and cumulative shielding duration through time-domain scanning with a fixed time step. To investigate aerodynamic effects, the model performs dynamic comparisons between drag-free flight at constant altitude and flight incorporating quadratic drag. The drag-inclusive model employs fourth-order Runge–Kutta numerical advancement. Results indicate: under no-drag conditions, the masking duration is 1.394 s with a minimum distance of 4.669 m; introducing quadratic drag increases masking duration to 1.809 s while reducing the minimum distance to 2.952 m, validating the positive gain from drag. The model converged through sensitivity analysis, demonstrating robust conclusions.

Downloads

Download data is not yet available.

References

[1] Ding Jialin, Chen Chunsheng, Li Qingwei, et al. Evaluation Indicators and Calculation Methods for Smoke Screen Interference Effectiveness [J]. Journal of Ordnance Engineering, 2024, 45(7):193-198.

[2] Zhang Chunhua, Xu Lixin, Zhang Yong. A Constraint-Based Interval Merging Algorithm [J]. Journal of Air Force University (Natural Science Edition), 2009 (04): 57-59.

[3] Guan Yixing. Intelligent Optimization Algorithms and Their Application in Missile Interception Task Allocation [D]. Harbin Institute of Technology, 2023.

[4] Yan Tian, Cheng Haoyu, Gao Mengjing, et al. Robust Intelligent Guidance Law for Missile Interception Based on Preset Performance [J]. Acta Astronautica Sinica, 2023.

[5] Sun Xue'an. Research on State Estimation and Cooperative Guidance Methods for Multi-Aircraft Missile Interception [D]. Nanjing University of Aeronautics and Astronautics, 2023.

Downloads

Published

28-02-2026

Issue

Section

Articles