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RANGE-ONLY INITIAL ORBIT DETERMINATION

机译:仅范围初始轨道确定

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Range-only initial orbit determination (IOD) is designed to derive six-dimensionalorbit estimates from range measurements, their time-tags, and sensor locations.Accurate range-rate interpolants are derived from range measurementswith a new interpolation algorithm that couples Lagrange and Chebyshevinterpolators. The IOD measurement set thus consists of range measurementsand range-rate interpolants. Reduction from the six dimensional orbit problemto a three dimensional problem is enabled with the use of Lagrange's f and gexpressions as developed by Herrick in closed form. A new three-dimensionalsearch algorithm calculates multiple six-dimensional orbit estimates usingtwo-body dynamics. The number of solutions was found to be inversely proportionalto the size of range measurement component thermal noise SigmaσW. Each two-body orbit estimate is used to seed an iterative nonlinear leastsquares orbit determination with full force model. Iterative convergence definessuccess for the range-only IOD estimate used.
机译:仅范围初始轨道确定(IOD)旨在得出六维 根据距离测量值,其时间标记和传感器位置估算轨道。 精确的距离率内插值是从距离测量得出的 结合了拉格朗日和切比雪夫的新插值算法 插补器。因此,IOD测量集包括范围测量 和范围率插值器。减少六维轨道问题 拉格朗日的f和g使一个三维问题成为可能 由Herrick开发的封闭形式的表达式。新的三维 搜索算法使用以下方法计算多个六维轨道估计值 两体动力学。发现解的数量成反比 到量程测量元件的大小热噪声西格玛 σW。每个两体轨道估计都用于播种迭代非线性最小 用全力模型确定平方轨道。迭代收敛定义 仅使用范围的IOD估算值是否成功。

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