Space target key feature identification method based on luminosity signal
A space target and identification method technology, applied in the key feature identification of space target based on photometric signal, and the field of space information detection, can solve the problems of long distance, low imaging resolution, difficulty in effectively obtaining space target features, etc.
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[0036] 1. Prediction of space target position and attitude
[0037] If the gravitational influence of other celestial bodies is ignored, and only the perturbation effect of the solar radiation pressure on the orbit of the space object is considered, the acceleration expression of the space object is
[0038]
[0039] In the formula, a per is the acceleration caused by solar radiation pressure, μ is the gravitational constant of the earth, and r is the distance from the space object to the center of the earth.
[0040] A quaternion is defined as
[0041] q=[q 0 mu T ] T
[0042] Among them, q 0 and μ are defined as
[0043]
[0044]
[0045] In the formula, ν is the Euler rotation angle, is the Euler axis of rotation.
[0046] Most space targets do not have the ability to adjust attitude and belong to the spin stabilization system. The spin-stabilized space target rotates at a constant speed around a fixed rotation axis, and the motion update model of its a...
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