DocumentCode :
1795078
Title :
Uncertainties simulation in hover/low speed for unmanned helicopter
Author :
Wang Yi ; Zeng Guogui ; Liao Zhilin ; Zu Jiakui
Author_Institution :
Coll. of Autom., Nanjing Univ. of Aeronaut. & Astronaut., Nanjing, China
fYear :
2014
fDate :
8-10 Aug. 2014
Firstpage :
1240
Lastpage :
1244
Abstract :
Uncertainties caused by modeling and flight of unmanned helicopter often simulated in the process of the control design. At present, many uncertainties are described by adding some easy little motion to the nonlinear model, which can´t be accurately reflected in the MATLAB. For the way, this paper advanced a way to describe the uncertainties base on the complex plant characteristic in hover/low speed of the unmanned helicopter. The uncertainties simulation model was developed on MATLAB. This method could reflect the uncertainties in hover/low speed of unmanned helicopter easily, quickly and correctly.
Keywords :
autonomous aerial vehicles; control system synthesis; helicopters; MATLAB; complex plant characteristic; nonlinear model; uncertainties simulation; unmanned helicopter; Aerodynamics; Equations; Force; Helicopters; Mathematical model; Rotors; Uncertainty;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
Conference_Location :
Yantai
Print_ISBN :
978-1-4799-4700-3
Type :
conf
DOI :
10.1109/CGNCC.2014.7007380
Filename :
7007380
Link To Document :
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