Title :
UAV glider control system based on dynamic contraction method
Author :
Bachuta, M.J. ; Czyba, R. ; Janusz, W. ; Yurkevich, V.D.
Abstract :
In this article two control structures for UAV (Unmanned Aerial Vehicle) glider are presented. Both structures are using control law based on dynamic contraction method, both of these are of cascade structure. Presented control systems allow to control aircraft yaw angle and velocity with respect to air. One of them also allows to stabilize sideslip angle on values close to zero. Proper operation of suggested structures is checked by using numerical simulation prepared in Matlab environment.
Keywords :
aircraft control; autonomous aerial vehicles; mathematics computing; numerical analysis; velocity control; Matlab environment; UAV glider control system; aircraft yaw angle control; control law; control structures; dynamic contraction method; numerical simulation; sideslip angle stabilization; unmanned aerial vehicle glider; velocity control; Aerodynamics; Aerospace control; Aircraft; Atmospheric modeling; Control systems; Equations; Mathematical model;
Conference_Titel :
Methods and Models in Automation and Robotics (MMAR), 2012 17th International Conference on
Conference_Location :
Miedzyzdrojie
Print_ISBN :
978-1-4673-2121-1
DOI :
10.1109/MMAR.2012.6347933
