A fast detection and positioning method for space debris based on a spaceborne visible light camera
A technology of space debris and positioning methods, which is applied in the directions of measuring devices, surveying and navigation, and photo interpretation, and can solve problems such as limited computing resources
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[0097] This embodiment discloses a method for quickly detecting and locating space debris based on a spaceborne visible light camera. To verify the method, firstly, a space debris image is simulated and generated. The basic parameters of the camera are shown in Table 1. according to Figure 6 The pinhole imaging model and the C-W equation are shown, and the motion state of the debris relative to the spacecraft in the camera coordinate system and the debris radius r at the initial moment are set as shown in Table 2. The spacecraft is running in a geosynchronous orbit. The first frame image obtained by the camera is as follows: Figure 8 Shown in the white box is a partial enlarged view.
[0098] Table 1 Basic parameters of camera
[0099]
[0100] Table 2 The initial relative motion state of fragments
[0101]
[0102]
[0103] Step 1: Number the debris trajectories in the pictures taken by the spaceborne visible light camera by means of connected domain detection....
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