A precise calculation method for the position of spaceborne GNSS-R specular reflection point
A specular reflection and calculation method technology, which is applied in satellite radio beacon positioning systems, measuring devices, instruments, etc., can solve the problem of accurately calculating the position deviation of specular reflection points, etc.
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[0039] In order to make the object, technical solution and advantages of the present invention clearer, the embodiments disclosed in the present invention will be further described in detail below in conjunction with the accompanying drawings.
[0040] Such as figure 1 , in an embodiment of the present invention, the method for accurately calculating the position of the satellite-borne GNSS-R mirror reflection point includes:
[0041] Step S1, according to the position point T of the GNSS satellite and the position point R of the receiver satellite, calculate and obtain the initial position point S which becomes the mirror reflection point.
[0042] In this embodiment, the initial position point S can be obtained by solving the following geometric relationship:
[0043] a) Relative vector according to point R The symmetry point U of , and the relative vector of point M The symmetry point C of is obtained by calculating the point M through the parallelogram rule.
[0044]...
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