A method for determining initial orbits of space targets under virtual coplanarity constraints
A technology for determining spatial objects and methods, which is applied in the interpretation of photos, etc., and can solve problems such as the joint adjustment of multi-frame images that cannot realize the calculation of spatial object positions
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[0063] The present invention will be further explained below in conjunction with the accompanying drawings and specific embodiments. The embodiments described in the present invention are only some of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, other embodiments obtained by persons of ordinary skill in the art without making creative efforts all fall within the protection scope of the present invention.
[0064] The invention establishes an observation platform motion compensation algorithm based on affine transformation, and constructs a static virtual coplanar condition observation model and a space-time joint initial orbit determination algorithm under the support of geometry and dynamics theory.
[0065] A method for determining the initial orbit of a space target under the constraints of a virtual coplanar condition according to the present invention comprises the following steps:
[0066] Step A: Use the ...
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