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