06.2 - Flight Dynamics and Control (UAV related)
LANDING SYSTEM USING EXTENDED DYNAMIC WINDOW APPROACH FOR FIXED-WING UAV
S. Ishioka¹, K. Uchiyama¹, K. Masuda¹; ¹Nihon University, Japan
We propose the extended Dynamic Window Approach that has low calculation load by solving the optimization problem to treat the number of restrictions on dynamics. The proposed method is applied to a landing system of a UAV considering restrictions of state variables and backside region. Numerical simulation and experiments will be conducted to verify its validity.