Title :
Modeling and Control for a Six-Rotor Aerial Vehicle
Author :
Yin, Liangliang ; Shi, Jingkui ; Huang, Yimin
Author_Institution :
Res. Inst. of Flight Control, Nanjing Univ. of Aeronaut. & Astronaut., Nanjing, China
Abstract :
In this paper, we have derived the linear model of a six-rotor aerial vehicle and proposed a controller for hovering. Attitudes of the six-rotor vehicle are affected by various sources of disturbances such as wind, measurement noise and modeling uncertainty. For these reasons, we proposed a controller based on disturbance observer, which estimates and compensates disturbances. It is shown by simulation that the proposed controller effectively rejects disturbances.
Keywords :
aircraft control; attitude control; modelling; observers; uncertain systems; disturbance observer; hovering control; linear model; modeling uncertainty; six-rotor aerial vehicle control; six-rotor aerial vehicle modelling; Equations; Mathematical model; Noise; Observers; Propellers; Vehicle dynamics; Vehicles; disturbance observer; dynamic model; hovering control; six-rotor; unmanned aerial vehicles(UAVs);
Conference_Titel :
Electrical and Control Engineering (ICECE), 2010 International Conference on
Conference_Location :
Wuhan
Print_ISBN :
978-1-4244-6880-5
DOI :
10.1109/iCECE.2010.320