01266nam a2200253 c 4500001001300000005001500013008004100028040001100069041001300080052002600093245020700119300003200326545005900358545005700417545005900474653015300533700005300686700003600739700004000775773014200815900002000957900001800977900001700995KSI00013578720040214190836031209s1997    ulka          000   eng    a0110010 aengbkor01a558.05b한642c25(1)00aFeedback control law design for dual spin turn maneuver of spacecraft=x위성체의 이중 회전 선회 기동을 위한 피이드백 제어법칙 설계/dHyo-Choong Bang,eSung-Kyu Kim,eHan Hwangbo  ap. 146-155:b삽도;c26 cm  aHyo-Choong Bag, 정회원, 한국항공우주연구소  aSung-Kyu Kim, 정회원, 한국항공우주연구소  aHan Hwangbo, 정회원, 한국통신위성사업본부  a위성체a이중a회전선회a기동a피이드백a제어법칙설계계aFeedbackaControlaLawaDesignaDualaSpinaTurnaManeuveraSpacecraft1 a방효충,g方孝忠,d1964-0KAC2016222454aut1 a김성규,d1949-0KAC2018470111 a황보한,g皇甫漢0KAC2020H61300 t韓國航空宇宙學會誌.d韓國航空宇宙學會.g25卷 1號(1997년 2월), p. 146-155q25:1<146w(011001)KSE199509707,x1225-134810aBag, Hyo-Choong10aKim, Sung-Kyu10aHwangbo, Han