The article studies the open loop
and closed loop systems for the improved converter. An improved
DC-DC boost converter is modeled and simulated using Matlab
R2013a.
The simulation and experimental results of the tow systems are
presented and co
mpared. The performance of the improved
converter is also compared with the conventional boost converter.The article studies the open loop
and closed loop systems for the improved converter. An improved
DC-DC boost converter is modeled and simulated using Matlab
R2013a.
The simulation and experimental results of the tow systems are
presented and compared. The performance of the improved
converter is also compared with the conventional boost converter.
The focal point of this thesis is design of a control system to achieve the stability of the
aircraft, by using a three-axis accelerometer sensor and a three-axis gyro. This thesis
aims to studying the quadrotor UAV, and depend this research as a base for subsequent
research on the various applications of this type of aircraft.
