DocumentCode :
627344
Title :
PID, LQR and LQR-PID on a quadcopter platform
Author :
Argentim, Lucas M. ; Rezende, Willian C. ; Santos, Paulo E. ; Aguiar, Renato A.
fYear :
2013
fDate :
17-18 May 2013
Firstpage :
1
Lastpage :
6
Abstract :
This paper aims to present a comparison between different controllers to be used in a dynamic model of a quadcopter platform. The controllers assumed in this work are an ITAE tuned PID, a classic LQR controller and a PID tuned with a LQR loop. The results were obtained through simulations for 10 different attitudes of the quadcopter, however, in this paper simulation results will be presented for the vertical attitude only (the remainder are analogous and were omitted for brevity).
Keywords :
autonomous aerial vehicles; linear quadratic control; robot dynamics; three-term control; ITAE tuned PID; LQR loop; LQR-PID; classic LQR controller; quadcopter platform dynamic model; unmanned aerial vehicles; vertical attitude; Aerospace electronics; Attitude control; Equations; Mathematical model; Transfer functions; Tuning; Vehicle dynamics;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Informatics, Electronics & Vision (ICIEV), 2013 International Conference on
Conference_Location :
Dhaka
Print_ISBN :
978-1-4799-0397-9
Type :
conf
DOI :
10.1109/ICIEV.2013.6572698
Filename :
6572698
Link To Document :
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