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