Integrated Guidance and Control Using Model Predictive Control with Flight Path Angle Prediction against Pull-Up

Jongho Park1, Youngil Kim2, Jong-Han Kim3

  • 1Department of Military Digital Convergence, Ajou University, Suwon 16499, Korea.

Summary

This study introduces an integrated guidance and control system using model predictive control for missile interception of maneuvering targets. The algorithm effectively estimates target motion and predicts future positions for enhanced interception capabilities.

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