Modeling for Landing Process of a Helicopter with Rotator Self-rotating based on Support Vector Machine

被引:1
作者
Wang, Shuzhou [1 ]
San, Ye [1 ]
Zhang, Yunchang [2 ]
机构
[1] Harbin Inst Technol, Control & Simulat Ctr, Harbin 150001, Peoples R China
[2] Flight Simulat Res Inst Air Force, Harbin 150001, Peoples R China
来源
2008 7TH WORLD CONGRESS ON INTELLIGENT CONTROL AND AUTOMATION, VOLS 1-23 | 2008年
关键词
support vector machine; helicopter; simulation model; generalization ability;
D O I
10.1109/WCICA.2008.4592998
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
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.
引用
收藏
页码:645 / +
页数:3
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