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METHOD FOR DETERMINING ORBIT OF DEEP SPACE SATELEITE AND DEEP SPACE NAVIGATION AIDING SATELITE
METHOD FOR DETERMINING ORBIT OF DEEP SPACE SATELEITE AND DEEP SPACE NAVIGATION AIDING SATELITE
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机译：确定深空卫星轨道的方法及深空导航辅助卫星
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摘要
PURPOSE: To improve accuracy in the determination of an orgit by disposing a deep space navigation aiding satelite as one flying on the orbit centering around the sun and utilizing the ranging path of the deep space satelite and earth through the deep space navigation aiding satelite to determine the orbit of the deep space satelite. ;CONSTITUTION: A deep space navigation aiding satelite 1 is disposed to fly on an orbit 5 centering around the sun 1 and provided with a function to range the earth 3 and a function to relay the ranging of the deep space satelite 2 and the earth 3. The satelite 1 observes the range data, range rate data and angular data by ranging along the ranging path 8 of the earth 3 satelite 2. Similar data are observed by the ranging along the ranging path 6 of the satelite 2 and the earth 3 through the deep space navigation aiding satelite 1 and the ranging along the ranging path 7 of the deep space navigation aiding satelite 1 and the earth 3 to determine the orbit of the satelite 2 on the basis of these data.;COPYRIGHT: (C)1996,JPO
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