Indian Journal of Science and Technology
Year: 2019, Volume: 12, Issue: 27, Pages: 1-4
S. Achmadi1, Miswanto2* and Marjono3
1National Institute of Technologi, Malang, Indonesia; [email protected]d
2Depatement Matematika, Universitas Airlangga, Surabaya, Indonesia; [email protected]
3Depatement Matematika, Universitas Brawijaya, Malang, Indonesia; [email protected]
*Author for correspondence
Depatement Matematika, Universitas Airlangga, Surabaya, Indonesia; [email protected]
Airplane should flight in compliance with the predetermined flight track to avoid the accident. This paper discusses how to design the optimal tracking control from airplanes with the influence of leader. There are four steps in designing the control of airplane’s movement by leader influence. Firstly, we will modify the airplane model by adopting Fossen model1 . Secondly, we determine the trajectory that will be tracked by the movement of airplanes. Thirdly, we design the control of airplane’s movement by using tracking error dynamics methods to the leader and the agents. Finally, the numerical simulation output is shown by error tracking of airplane’s movement towards desired path followed by agents and leader of the planes.
Keywords: Error Tracking, Numerical Simulation, Plane Model, Tracking,
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