发明名称 METHOD OF ORIENTATION OF SPACECRAFT
摘要 FIELD: programmed positioning and orientation of mobile objects; angular orientation or positioning of spacecraft. ^ SUBSTANCE: proposed method includes measurement of angles of position of optical axes of astro-visual units tracking the stars relative to body-axis coordinate system. For determination of orientation of mobile object, use is made of coordinates of its center of mass in geocentric coordinate system which are determined by means of high-precision global navigation satellite system. ^ EFFECT: enhanced accuracy of orientation of mobile objects. ^ 2 dwg
申请公布号 RU2247945(C1) 申请公布日期 2005.03.10
申请号 RU20030117285 申请日期 2003.06.09
申请人 发明人 ANANENKO V.M.;SMIRNOV V.V.;SHEVCHENKO P.V.
分类号 G01C21/24 主分类号 G01C21/24
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