Method for determining signal-to-noise ratio of optical remote sensor by combining satellite orbit characteristics
A technology for optical remote sensors and satellite orbits, which is applied in the field of aerospace optical remote sensing, and can solve problems that have not yet been raised
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[0051] Such as figure 1 Shown, the realization process of the present invention is:
[0052] (1) The satellite moves along the conic curve, the focus F of the conic curve is located at the center of the earth, then the orbital equation of the satellite is written as the earth center distance r as:
[0053] r = a ( 1 - e 2 ) 1 + e cos f
[0054] The relationship between satellite anomaly E and true anomaly f is:
[0055] acosE=ae+rcosf
[0056] bsinE=rsinf
[0057] Derived to get:
[0058] cos E = e - cos f 1 + e cos f ...
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