01197na  a2200217   4500001001300000005001500013008004100028041001300069052002600082245023700108300002100345545006500366545006500431546002500496653021900521700001900740700004800759773013900807900001700946900001600963KSI00095819720190927102318190819s2019    ulk           000   kor  0 akorbeng01a558.05b한642c47(1)00a광학식 3차원 좌표측정장치를 이용한 관성항법센서와 기체의 정렬기법 =xAlignment of inertial navigation sensor and aircraft fuselage using an optical 3D coordinate measuring device /d김정호,e이대우  ap. 41-48 ;c26cm  a김정호, Aerospace department of Pusan National University  a이대우, Aerospace department of Pusan National University  a영어 요약 있음  a센서 정렬a최적화a절대 표정a관성항법시스템a광학식 좌표측정장치aSensor alignmentaOptimizationaAbsolute orientationaInertial navigation systemaOptical coordinate measurement machine1 a김정호4aut1 a이대우,g李大雨,d1969-0KAC2018270430 t韓國航空宇宙學會誌.d韓國航空宇宙學會.g47권 1호(2019년 1월), p. 41-48q47:1<41w(011001)KSE199509707,x1225-134810aKim, Jeongho10aLee, Daewoo