01312nam a2200253 c 4500001001300000005001500013008004100028040001100069041001300080052002600093245019200119300002100311545009700332545007900429545007900508653017000587700005300757700001400810700003600824773014200860900001901002900001801021900001901039KSI00062680720071017103453070720s2005    ulk           000   kor    a0110010 akorbeng01a558.05b한642c33(2)00a3단형 발사체 TVC 자세제어 설계 및 분석=xAttitude control design and analysis for thrust vector control system of 3-staged launch vehicle/d선병찬,e박용규,e최형돈  ap. 67-74;c26 cm  a선병찬, 정회원, 한국항공우주연구원 우주발사체사업단bbcsun@kari.re.kr  a박용규, 정회원, 한국항공우주연구원 우주발사체사업단  a최형돈, 정회원, 한국항공우주연구원 우주발사체사업단  a발사체a자세제어a안정성 분석a벤딩필터a비례-미분 제어기aLaunch vehicleaAttitude controlaStability analysisaBending filteraPD controller1 a선병찬,g宣炳纂,d1968-0KAC2017052694aut1 a박용규1 a최형돈,d1958-0KAC2017083240 t韓國航空宇宙學會誌.d韓國航空宇宙學會.g제33권 2호(2005년 2월), p. 67-74q33:2<67w(011001)KSE199509707,x1225-134810aSun, Byungchan10aPark, Yongkyu10aChoi, Hyungdon