DocumentCode :
3203866
Title :
PID vs. MRAC Control Techniques Applied to a Quadrotor´s Attitude
Author :
Yong Zeng ; Qiang Jiang ; Qiang Liu ; Hua Jing
Author_Institution :
Sch. of Aeronaut. & Astronaut., UESTC, Chengdu, China
fYear :
2012
fDate :
8-10 Dec. 2012
Firstpage :
1086
Lastpage :
1089
Abstract :
Attitude is the key parameters for a Quadrotor. This paper designed a Proportional Integral Differential (PID) controller and a Model Reference Adaptive Control (MRAC) controller for a Quadrotor. At the end, a simulation was introduced. The simulation result told that MRAC controller had the ability to avoid the noise with the power such as 0.01.
Keywords :
machine control; model reference adaptive control systems; rotors; three-term control; MRAC control techniques; PID control techniques; model reference adaptive control; proportional integral differential controller; quadrotor attitude; Adaptation models; Attitude control; Equations; Helicopters; Mathematical model; Noise; Rotors; MRAC; PID; Quadrotor;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Instrumentation, Measurement, Computer, Communication and Control (IMCCC), 2012 Second International Conference on
Conference_Location :
Harbin
Print_ISBN :
978-1-4673-5034-1
Type :
conf
DOI :
10.1109/IMCCC.2012.256
Filename :
6429092
Link To Document :
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