A Model Based Flight Control System Design Approach for Micro Aerial Vehicle Using Integrated Flight Testing and HIL Simulation
AIAA Scitech 2019 Forum, San Diego, CA/AMERİKA BİRLEŞİK DEVLETLERİ, 7 Ocak 2019
YÜKSEK BURAK, SALDIRAN EMRE, YENİÇERİ RAMAZAN, İNALHAN GÖKHAN