DocumentCode
2476664
Title
Modeling for landing process of a helicopter with rotator self-rotating based on support vector machine
Author
Wang, Shuzhou ; San, Ye ; Zhang, Yunchang
Author_Institution
Control & Simulation Centre, Harbin Inst. of Technol., Harbin
fYear
2008
fDate
25-27 June 2008
Firstpage
645
Lastpage
649
Abstract
As a system identification method, neural network can be applied to build the simulation model of a helicopter. But it has some difficulties such as the hardness of selecting network structure, slow convergence speed, local minimum, and generalization ability question. To avoid the question above, the support vector machine (SVM) method is introduced to the field of flight simulation for the first time, and the rotator speed model for landing process of a helicopter with rotator self-rotating is built. Compared with the neural network model, the SVM simulation model of a helicopter owns some advantages such as simple structure, fast convergence speed and high generalization ability. It is shown by theoretic analysis and simulation result that the SVM method is feasible.
Keywords
helicopters; identification; neurocontrollers; support vector machines; helicopter landing process; neural network; rotator speed model; selecting network structure hardness; support vector machine; system identification method; Aerospace simulation; Automation; Convergence; Electronic mail; Force control; Helicopters; Intelligent control; Neural networks; Support vector machines; System identification; generalization ability; helicopter; simulation model; support vector machine;
fLanguage
English
Publisher
ieee
Conference_Titel
Intelligent Control and Automation, 2008. WCICA 2008. 7th World Congress on
Conference_Location
Chongqing
Print_ISBN
978-1-4244-2113-8
Electronic_ISBN
978-1-4244-2114-5
Type
conf
DOI
10.1109/WCICA.2008.4592998
Filename
4592998
Link To Document