06.1 - Flight Dynamics and Control (Control & Modelling)
PURSUIT-BASED LONG-RANGE AIR-TO-AIR MISSILE MIDCOURSE GUIDANCE ROBUST TO CHANGES IN THE PREDICTED IMPACT POINT
M. Shin¹, M.-J. Tahk¹, B. Kim¹, C.-H. Lee¹; ¹Korea Advanced Institute of Science and Technology, South Korea
This paper proposes a midcourse guidance method that is robust to changes in the predicted impact point (PIP). The guidance method consists of a reference trajectory with an altitude constraint and a pursuit-based guidance that follows the reference trajectory. Simulation results show that the proposed guidance method is significantly robust to changes in the PIP.