진화 알고리듬을 이용한 항공기 제어기 설계 Aircraft Control System Design Using Evolutionary Algorithm

An aircraft acceleration control system is designed using various evolutionary algorithms. Evolution strategies are used to find the optimal gains for the controller. We also apply co-evolutionary algorithm in finding the saddle point solutions for the same system. Worst-case evolutionary algorithm is proposed for designing a robust controller. In the proposed algorithm, one group co-evolves while the other group simulates a random behavior. The evolving group is able to find a robust value for the search space. The solutions and properties of three methods are compared and analyzed.
Publisher
한국항공우주학회
Issue Date
1999-01
Language
KOR
Citation

한국항공우주학회지, v.27, no.4, pp.104 - 114

ISSN
1225-1348
URI
http://hdl.handle.net/10203/71455
Appears in Collection
AE-Journal Papers(저널논문)
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