Dual-satellite positioning method based on WGS (World Geodetic System)-84 model
A WGS-84, positioning method technology, applied in satellite radio beacon positioning systems, measuring devices, instruments, etc., can solve problems such as positioning solution ambiguity, inability to uniformly solve satellite co-orbit/different orbit, and iterative methods to solve problems such as difficulty
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[0088] The following is a verification and description of the above-mentioned closed solution algorithm scheme for direction finding and positioning based on the WGS-84 earth ellipsoid model constrained by the accompanying drawings. First, the following reasonable assumptions are made for the system model:
[0089] 1. Assume that the double star is a low-orbit satellite, and the orbital height is relatively low, usually 500km to 1000km;
[0090] 2. Unify the satellite attitude measurement error existing in engineering practice into the satellite direction finding error;
[0091] 3. Assume that the measurement errors obey a Gaussian distribution with a mean of zero, and the errors are independent of each other.
[0092] (1) Positioning effect when double stars are in different orbits:
[0093] Such as figure 2 As shown, it is assumed that the binary star is an out-of-orbit binary star, and the orbit heights are H S1 =500km,H S2 =550km, the corresponding satellite sub-satel...
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