DocumentCode :
3163904
Title :
Trajectory-tracking control design and modeling for quadrotor aerial vehicles
Author :
Margun, Alexey ; Bazylev, Dmitry ; Zimenko, Konstantin ; Kremlev, Artem
Author_Institution :
Fac. of Comput. Technol. & Control, ITMO Univ., St. Petersburg, Russia
fYear :
2015
fDate :
16-19 June 2015
Firstpage :
273
Lastpage :
277
Abstract :
A control algorithm for finite-time tracking of quadrotor is introduced. The algorithm is based on use of feedback linearization method and finite-time output control presented in [17]. In comparison with commonly used in practice control methods like PD-controller the proposed method allows to estimate the first derivatives of the generalized coordinates, that enable to reduce the number of necessary sensors and thereby reduce the cost of the quadrotor. Moreover, the method is robust with respect to external disturbances and discretization that is useful for quadrotor control due to operating in open areas and digitality of sensors and controller. The performance and effectiveness of the method is demonstrated by simulation results of the system with external perturbations and signal discretization.
Keywords :
control system synthesis; feedback; helicopters; linearisation techniques; perturbation techniques; robust control; trajectory control; external perturbations; feedback linearization method; finite-time output control; quadrotor aerial vehicles; quadrotor finite-time tracking; robust control; signal discretization; trajectory-tracking control design; Control design; Mathematical model; Robots; Robustness; Sensors; Stability analysis; UAV; finite-time control; quadrotor; robust control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control and Automation (MED), 2015 23th Mediterranean Conference on
Conference_Location :
Torremolinos
Type :
conf
DOI :
10.1109/MED.2015.7158762
Filename :
7158762
Link To Document :
بازگشت