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무인기 유도제어시스템 설계 및 비행시험을 통한 성능 검증 : Design and performance verification of UAV control system via flight test
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- Authors
- Advisor
- 김유단
- Issue Date
- 2007
- Publisher
- 서울대학교 대학원
- Keywords
- 무인항공기 ; UAV ; 유도제어시스템 ; guidance control system ; 선형최적제어 ; linear quadratic regulator ; 적응제어 ; adaptive control ; HILS ; HILS ; 비행시험 ; flight test
- Description
- 학위논문(석사)--서울대학교 대학원 :기계항공공학부,2007.
- Language
- Korean
- URI
- http://dcollection.snu.ac.kr:80/jsp/common/DcLoOrgPer.jsp?sItemId=000000045738
https://hdl.handle.net/10371/48183
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