Development Of The Unmanned Aerial Vehicle In Hexacopter For Attitude Control

Wong, Yew Moon (2017) Development Of The Unmanned Aerial Vehicle In Hexacopter For Attitude Control. Project Report. Universiti Teknikal Malaysia Melaka, Melaka, Malaysia. (Submitted)

Text (24 Pages) Development Of The Unmanned Aerial Vehicle In Hexacopter For Attitude Control.pdf - Submitted Version Download (836kB)

Abstract

Unmanned aerial vehicles (UAVs) nowadays has become increasingly common application in military options, surveillance,meteorological investigation and robotics research especially multi-copter.Hexacopter is a type of multi copter which has high stability due to it possibility manage one or more engine failure and increase the total payload.The attitude of the hexacopter is implemented by PID controller in APM as microcontroller to tune for good stability control in angular velocity.The mathematic model presented by considering all its external and influences.It is well known that,assume the multi copter as a rigid body,its dynamic behaviour described from the differential equations derived from the Euler-Lagrange equations leading to equivalent mathematical model are programed into Arduino for control the algorithm.Lastly,the hardware and software combined all together.With developed the control algorithm in hexacopter was controlled by using RC controller which more user friendly interface when doing the data analysis on test pad with Mission Planner under indoor environment due to neglect all the disturbance for investigate the attitude performance of developed hexacopter.

Actions (login required)

View Item