I. Introduction
In recent decades, the use of quadrotor unmanned aerial vehicles (UAVs) has increased in surveillance, rescue, and reconnaissance tasks [1], [2], [3], due to their compact structure and portability. Since the endurance capacity of quadrotor UAVs is limited, frequent recovery is necessary during air missions. Consequently, autonomous landing control of quadrotor UAVs has become a crucial research topic, with applications that extend to tracking ground targets and collaborative ground–air operations [4], [5].