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Precise Analytical Computation of Frozen-Eccentricity, Low Earth Orbits in a Tesseral Potential

机译:卫星偏位势中冻结偏心率低地球轨道的精确解析计算

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Classical procedures for designing Earth's mapping missions rely on a preliminary frozen-eccentricity orbit analysis. This initial exploration is based on the use of zonal gravitational models, which are frequently reduced to a simple J_2-J_3 analysis. However, the J_2-J_3 model may not be accurate enough for some applications. Furthermore, lower order truncations of the geopotential are known to fail in describing the behavior of elliptic frozen orbits properly. Inclusion of a higher degree geopotential, which also takes into account the short-period effects of tesseral harmonics, allows for the precise computation of frozen-eccentricity, low Earth orbits that show smaller long-period effects in long-term propagations than those obtained when using the zonal model design.
机译:设计地球测绘任务的经典程序依赖于初步的冻结偏心率轨道分析。最初的探索基于区域重力模型的使用,该模型通常简化为简单的J_2-J_3分析。但是,J_2-J_3模型对于某些应用程序可能不够准确。此外,已知地势的低阶截断未能正确地描述椭圆形冻结轨道的行为。包含更高程度的地势,这也考虑了地基谐波的短周期影响,可以精确计算出冻结偏心率,低地球轨道,该轨道在长期传播中显示的长期影响小于使用分区模型设计。

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  • 来源
    《Mathematical Problems in Engineering 》 |2013年第2期| 191384.1-191384.13| 共13页
  • 作者单位

    C/Columnas de Hercules 1,11100 San Fernando, Spain;

    Departamento de Matematicas y Computation, Universidad de La Rioja, 26004 Logrono, Spain;

    Departamento de Ingenieria Mecanica, Universidad de La Rioja, 26004 Logrono, Spain;

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