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    • 1. 发明申请
    • ANGLES-ONLY INITIAL ORBIT DETERMINATION (IOD)
    • 角度唯一的初始轨道确定(IOD)
    • WO2015065641A1
    • 2015-05-07
    • PCT/US2014/058621
    • 2014-10-01
    • RAYTHEON COMPANYCOLEMAN, Gary D.SILNY, John F.
    • COLEMAN, Gary D.SILNY, John F.
    • B64G1/24B64G3/00
    • B64G3/00B64G1/242
    • A methodology for initial orbit determination of an object about an astronomical body searches a grid of possible boundary values on the range-to-object over the observation interval to find the grid point and corresponding initial orbit that best fits all of the three or more (N) angles-only observations according to an error metric. The search is conducted by solving a boundary-value problem (e.g. Lambert's Problem) for different grid points. The state vector is propagated to determine estimated observation directions for the remaining N-2 observations. The grid point (and initial orbit) that best fit all of the observations is selected. The grid may be searched by testing each and every point on the grid or by using other optimization techniques such as hill climbing algorithms to find the optimal grid point.
    • 关于天文体的物体的初始轨道确定的方法在观察间隔上搜索在距离对象上的可能边界值的网格,以找到最适合所有三个或更多个的网格点和对应的初始轨道( N)根据误差度量的仅角度观测值。 搜索通过解决不同网格点的边界值问题(例如朗伯问题)进行。 传播状态矢量以确定剩余N-2观测值的估计观察方向。 选择最适合所有观测值的网格点(和初始轨道)。 可以通过测试网格上的每个点或通过使用其他优化技术(如爬山算法)来找到最佳网格点来搜索网格。