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Simulation and Experimental Works of Quadcopter Model for Simple Maneuver

By Rafiuddin Syam and Mustari Mustari

Abstract

This study aims to create a simulated and experimental of aircraft movements for multirotor quadcopter. The research method is theoretical and experimental methods. For theoretical method consists of calculating the dynamics and kinematics. While the experimental method consists of the aircraft testing and processing of GPS data recorded aircraft. The results showed that the acceleration acting on the aircraft is large enough that x ̈ = 1.751 m/s2, y = 2.038 m /s2 = 1.6371 m danz ̈ / s2, (2) the value of the maximum error between the theoretical and the actual movement is ex = 0.682 m; ey and ez = 0.353 m = 0.546 m. Theoretical movement pattern already resembles the actual movemen

Topics: model simulation, quadcopter, dynamic control, kinematics control, Technology, T, Electrical engineering. Electronics. Nuclear engineering, TK1-9971, Materials of engineering and construction. Mechanics of materials, TA401-492
Publisher: Hasanuddin University
Year: 2017
OAI identifier: oai:doaj.org/article:55acfb97accd46a592c88530e9e27e63
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