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A Comparison of Theory and Observation of the Echo I Satellite

机译:回声一号卫星理论与观测的比较

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摘要

Observations of the Echo I balloon satellite have been compared with a theory including the following perturbing effects: (1) solar radiation pressure; (2) lunar and solar gravitation; (3) second, third, and fourth harmonics of the earth's gravitational potential; and (4) atmospheric drag. With a set of orbital elements at the 26th day of the lifetime of the satellite, it was possible to match the observational data to 180 days with root mean square residuals as follows: Delta-a = 17.9 km, Delta-e = 0.0021, Delta-i = 0.0177 deg., Delta-omega = 1.1231 deg., Delta-Omega = 0.4821 deg., Delta-perigee height = 7.50 km. No differential correction has been applied as yet. Values of atmospheric density between 1500 and 930 km, assuming neutral drag effects only, have been inferred from the orbital data. The connection between solar activity and drag is also examined. As the Echo I perigee height continues to oscillate between 900 and 1500 km, more valuable orbital data will be obtained and atmospheric properties will be deduced. Further refinements in the mathematical model, especially in a time-dependent model atmosphere, should bring a substantial reduction in the residuals of the observations.
机译:已经将回声一号气球卫星的观测结果与包括以下扰动效应的理论进行了比较:(1)太阳辐射压力; (2)月球和太阳引力; (3)地球重力势的二次,三次和三次谐波; (4)大气阻力。在卫星生命周期的第26天使用一组轨道元素,可以将观测数据与180天相匹配,均方根残差如下:Delta-a = 17.9 km,Delta-e = 0.0021,D​​elta -i = 0.0177度,Δ-ω= 1.1231度,Δ-ω= 0.4821度,近地角高度= 7.50 km。尚未应用差分校正。仅从中性阻力效应出发,已经从轨道数据中推断出了1500至930 km之间的大气密度值。还研究了太阳活动与阻力之间的联系。随着“回声一号”近地点高度持续在900至1500公里之间波动,将获得更多有价值的轨道数据,并推论出大气特性。数学模型的进一步完善,尤其是在与时间有关的模型气氛中,应会大大减少观测值的残差。

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    Bryant, R. W.;

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  • 年度 1961
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