Simulation and Experimental Works of Quadcopter Model for Simple Maneuver

Autor:	Rafiuddin Syam, Mustari Mustari
Jazyk:	angličtina
Rok vydání:	2017
Předmět:	model simulation quadcopter dynamic control kinematics control Technology Electrical engineering. Electronics. Nuclear engineering TK1-9971 Materials of engineering and construction. Mechanics of materials TA401-492
Zdroj:	International Journal on Smart Material and Mechatronics, Vol 2, Iss 1, Pp 29-33 (2017)
Druh dokumentu:	article
ISSN:	2356-5314 2460-075X
Popis:	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 movement
Databáze:	Directory of Open Access Journals
Externí odkaz:	https://doaj.org/article/55acfb97accd46a592c88530e9e27e63 Zobrazit plný text záznamu View record in DOAJ