05.2 - Flight Dynamics and Control (UAV related)
GUIDANCE AND CONTROL OF AUTOMATIC SHORT LANDING WITH STEEP GLIDE SLOPE FOR UAV
J. Moon¹, S. Choi¹, S. Cho¹, H. Kim¹; ¹KOREANAIR, South Korea
This paper represent guidance and control law used in the tactical UAV to perform automatic short landing with steep landing slope. Automatic landing system is utilized with ground and airborne precise tracking radar equipment to follow accurate landing trajectory. Performance of the automatic landing control law was verified with HILS and flight test.