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Design of waypoint guidance law with flight envelope protection for quadrotor unmanned aerial vehicle : 비행영역 보호를 고려한 쿼드로터 무인비행체의 유도기법 설계

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Authors

이상현

Advisor
김유단
Major
기계항공공학부
Issue Date
2011-08
Publisher
서울대학교 대학원
Keywords
쿼드로터무인항공기궤환선형화비행영역보호역오일러각UAVFeedback linearizationPeak response estimationFlight envelope protectionInverse Euler angles
Description
학위논문 (석사)-- 서울대학교 대학원 : 기계항공공학부, 2011.8. 김유단.
Language
eng
URI
https://hdl.handle.net/10371/157397

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