DocumentCode
3701518
Title
Improvement of quadrocopter command performance system
Author
Sergey Zavadskiy;Daria Sharovatova
Author_Institution
St. Petersburg State University, 7/9 Universitetskaya nab., 199034 Russia
fYear
2015
Firstpage
609
Lastpage
610
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"
Publisher
ieee
Conference_Titel
"Stability and Control Processes" in Memory of V.I. Zubov (SCP), 2015 International Conference
Type
conf
DOI
10.1109/SCP.2015.7342220
Filename
7342220
Link To Document