Farhan Syafiq Rizqullooh Lubis

Design and Simulation of Harmonic Control for a Rolling Airframe R-Han 122 Surface-to-Surface Missile Using MATLAB–X-Plane Integration

Rolling motion in airframe missiles improves gyroscopic stability but may also induce control coupling and oscillatory responses that reduce flight stability. This study aims to design and evaluate a harmonic control strategy for the R-Han 122 surface-to-surface missile by integrating MATLAB and X-Plane 10. A numerical...