000 00719nam a22002057a 4500
003 OSt
040 _cIIT Kanpur
041 _aeng
082 _aNASA
_bTN D-1969
100 _aAdams, James J.
245 _aSimulator study of a satellite attitude control system using inertia wheels and a magnet [NASA TN D-1969]
_cJames J. Adams, W. E. Howell and Hugh P. Bergeron
260 _aWashington, D.C.
_bNational Aeronautics and Space Administration [NASA]
_c1963
300 _a16p
440 _aNational Aeronautics and Space Administration [NASA]
500 _aBound with NASA TN D-1961-1970. Lack No.-1966
650 _aInertia wheels
700 _aHowell, W. E.
700 _aBergeron, Hugh P.
942 _cTR
999 _c564516
_d564516