DocumentCode :
1795112
Title :
Unmanned helicopter control based on trim predication technology
Author :
Zhirong Lei ; Long Shi ; Jia Li ; Dongliang Song
Author_Institution :
Sch. of Autom., Northwestern Polytech. Univ., Xian, China
fYear :
2014
fDate :
8-10 Aug. 2014
Firstpage :
1368
Lastpage :
1372
Abstract :
This paper discusses the application of trim prediction technology which is used to design unmanned helicopter control laws. Trim prediction technology takes “implicit integrator” replace integrator appears explicitly in the PID control laws. For the first time, this paper adopts and applys the trim prediction technology to design unmanned helicopter control laws. According to simulation results, compared with traditional PID control laws, the simulation results are similar with PID control, but trim prediction technology can overcome disadvantages of traditional PID. The effectiveness of trim prediction control laws is documented through simulation. and shows that trim prediction technology can be used on unmanned helicopter.
Keywords :
aircraft control; autonomous aerial vehicles; control system synthesis; helicopters; position control; three-term control; PID control law; implicit integrator; trim predication technology; unmanned helicopter control; Attitude control; Computers; Helicopters; PD control; Real-time systems; Software;
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.2014.7007396
Filename :
7007396
Link To Document :
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