06.1 - Flight Dynamics and Control (Control & Modelling)
DOWNRANGE CONTROL GUIDANCE FOR REENTRY BURN OF REUSABLE LAUNCH VEHICLE
K.-W. Jung¹, C.-H. Lee¹; ¹KAIST, South Korea
This study addresses trajectory correction for Reusable Launch Vehicles using a new guidance law. It focuses on reentry burn phase, utilizing prediction of aero-ballistic trajectories by partial-closed form solution . Simulations confirm its effectiveness and computational efficiency, improving robustness of the RLV operations.