This project presents a control approach to obtain the better stabilization in attitude and altitude of quad-rotor under different disturbance conditions. In the standard Quad-rotor rotor type UAV, controlling of attitude and altitude is one of the most critical tasks and appropriate controller for stabilization of UAV is essential and necessary. Micro air vehicles (MAVs) have a wide application such as the military reconnaissance, meteorological survey, environmental monitoring, and other aspects. In this project, attitude and altitude control for Quad-Rotor type UAVs is discussed and analyzed. For the attitude control, a new method by using a gyroscope and a triaxial accelerometer is proposed to estimate the attitude angle information.
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