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Verification of GPS/INS for the SmartUAV using Aircraft Flight Test and Automobile Road Test  

Chang, Sung-Ho (한국항공우주연구원 스마트무인기사업단 무인체계팀)
Yoo, Jang-Sik ((주)마이크로인피니티)
Gwak, Min-Gyu ((주)마이크로인피니티)
Hong, Jin-Seok ((주)마이크로인피니티)
Publication Information
Aerospace Engineering and Technology / v.10, no.2, 2011 , pp. 1-10 More about this Journal
Abstract
This is a comparative study of three inertia navigation units and focuses on the verification of reliability about GPS/INS for the SmartUAV(DGNS). Those GPS/INS have been tested using a manned aircraft and an automobile. The comparative aspect of units include details about the GPS positions and the inertia sensor performance. With the flight scenario, the DGNS guarantees the reliability of the navigation operation and performs the flight test for the development of the SmartUAV.
Keywords
unmanned aircraft system, UAS; global positioning system and inertial navigation system; GPS/INS; flight test; road test;
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
연도 인용수 순위
1 장성호, 김영민, "상용 기성품에 기반한 스마트무인기 탑재자료저장장치", 항공우주기술, 제9권, 제2호, 2010, pp.153-160
2 Athena 511-300 FCS/INS User's manual, SYS-07-047, Rockwell Collins, Inc., October 2010.