Title :
Improvement of quadrocopter command performance system
Author :
Sergey Zavadskiy;Daria Sharovatova
Author_Institution :
St. Petersburg State University, 7/9 Universitetskaya nab., 199034 Russia
Abstract :
It is considered the problem of quadrocopter flight control. A system with four degrees of freedom is used as a model of the control object. Phase states of this system are acceleration along the vertical axis and Euler angles angular rate. Copter´s cxecutive system is improved by the addition of a filter. The step response of the system with filter is presented. Quality performance management system with simple PI regulator and with designed dynamic filter is demonstrated.
Keywords :
"Optimization","Conferences","Particle beams","Vehicle dynamics","Observers","Acceleration"
Conference_Titel :
"Stability and Control Processes" in Memory of V.I. Zubov (SCP), 2015 International Conference
DOI :
10.1109/SCP.2015.7342220
