A Feedback Linearization Approach for Path Trajectory Tracking of Quadrotor
محل انتشار: شانزدهمین کنفرانس بین المللی انجمن هوافضای ایران
سال انتشار: 1395
نوع سند: مقاله کنفرانسی
زبان: انگلیسی
مشاهده: 504
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شناسه ملی سند علمی:
AEROSPACE16_244
تاریخ نمایه سازی: 13 شهریور 1396
چکیده مقاله:
Unmanned aerial vehicles (UAVs) are being used more often for military and civilian purposes such as traffic monitoring, patrolling for forest fires, surveillance, and rescue, in which risks to pilots are often high. Rotorcraft have an evident advantage over fixed-wing aircraft for various applications because of their vertical landing/take-off capability and payload. Among the rotorcraft, quadrotor can usually afford a larger payload than conventional helicopters due to four rotors. Designing auto pilot with the aim of doing autonomously the desired missions can be introduced as an important field of quadrotors investigations. In this work, trajectory tracking of a quadrotor UAV is obtained by controlling attitude and position. Where, the Feedback Linearization method is used. As a first step, nonlinear 6 DOF dynamic model of quadrotor is presented. Then, Feedback Linearization (FBL) method is utilized for redefining the linearized dynamic model. Then, with the aim of being capable to stabilize and track the desired path trajectories, an Inverse Dynamic Controller is proposed. At last, a mission is designed and simulated to propose the application rate of designed controller.
کلیدواژه ها:
Quadrotor- Trajectory tracking- Nonlinear Controller- Feedback Linearization
نویسندگان
Alireza Radmanesh
Aerospace Engineering Department, Amirkabir University of Technology, Tehran, Iran
Abolghasem Naghash
Aerospace Engineering Department, Amirkabir University of Technology, Tehran, Iran