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Modeling of Guidance Mechanism for SACLOS ATGM and Simulation of Proportional-Derivative Coefficient Optimization

  • Journal of The Korea Society of Computer and Information
  • Abbr : JKSCI
  • 2026, 31(1), pp.283~291
  • Publisher : The Korean Society Of Computer And Information
  • Research Area : Engineering > Computer Science
  • Received : December 4, 2025
  • Accepted : December 29, 2025
  • Published : January 30, 2026

Kyuhong Choi 1 Jeong-Hyeon Moon 1 Min-Sue Hong 1 Hyun-Geun Yu 1

1한화시스템

Accredited

ABSTRACT

This paper systematically models the guidance mechanism of a second-generation wired Semi-Automatic Command to Line of Sight (SACLOS) anti-tank guided missile (ATGM) and conducts simulations against both stationary and moving targets. A stepwise velocity profile was defined up to a maximum range of 2000 m to establish realistic flight conditions. The feedback control structure of the SACLOS system was implemented, and missile guidance trajectories were reproduced based on this framework. In particular, for moving targets, the optimal proportional-derivative coefficients were inductively derived according to target speed and distance conditions to improve hit probability. Therefore, this study quantitatively verifies the guidance performance of SACLOS anti-tank missiles and demonstrates that optimizing proportional-derivative coefficients is critical to enhancing hit probability.

Citation status

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