00990nam a2200205 c 4500001001300000005001500013008004100028041001300069049003200082052001600114056001400130082001500144245021500159260003600374300003100410502008600441653017800527700005300705963002600758KDM20015668120020205135742020204s2001    ulka       AK 000   kor  0 akorbeng0 lEM2465354lEM2465355c2fDP01a558.92b1-1  a558.92240 a629.4722100a위성발사체의 궤적최적화와 관성유도 알고리듬 설계에 관한 연구=x(A)study on the trajectory optimization and inertial guidance algorithm design for satellite launch vehicles/d노웅래  a서울:b서울대학교,c2001  axiv, 175p.:b삽도;c26cm1 a학위논문(박사) --b서울대학교 대학원:c항공우주공학과,d2001  a위성발사체a궤적최적화a발사체a궤적a관성유도a알고리듬aTRAJECTORYaOPTIMIZATIONaINERTIALaGUIDANCEaALGORITHMaDESIGNaSATELLITEaLAUNCHaVEHICLES1 a노웅래,g盧雄來,d1967-0KAC2016345714aut  a항공우주공학과