A real-time tracking method for space dynamic target with multi-satellite coordination
A dynamic target and real-time tracking technology, applied in the field of satellite scheduling, can solve the problems of ignoring the real-time nature of tracking tasks, ignoring the rules of continuous resource usage on the satellite, and difficult identification
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Publication Date
- 2020-06-09
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Abstract
Description
technical field
[0001] The invention relates to the technical field of satellite scheduling, in particular to a multi-satellite coordinated space dynamic target real-time tracking method. Background technique
[0002] The real-time tracking task for ballistic missiles is an important means to discover, monitor and track enemy strategic missiles and issue alarms. It can obtain the infrared radiation of enemy strategic missiles, determine the coordinates of the missile's location, and judge the launch point and landing point of the missile , and can send target images to ground stations or ground command centers, providing important intelligence information for military anti-missile and military confrontation.
[0003] Space reconnaissance and surveillance systems usually include high-orbit satellites and low-orbit satellites. After the high-orbit satellite confirms the suspicious missile target, the ground command center dispatches the spaceborne staring detector on the low-...
Examples
Embodiment Construction
[0107] The following is a detailed description of the embodiments of the present invention. This embodiment is carried out based on the technical solution of the present invention, and provides detailed implementation methods and specific operation processes to further explain the technical solution of the present invention.
[0108] A multi-satellite coordinated space dynamic target real-time tracking method of the present invention includes two stages: tracking task decomposition based on rolling time domain and multi-satellite coordinated reconnaissance task scheduling, such as figure 1 , 2 As shown, it specifically includes the following steps:
[0109] Step 1, establish a problem model;
[0110] In view of the characteristics of high real-time tracking tasks, difficult recognition, and fine time constraints, in the tracking task decomposition stage, the problem model is firstly established, including low-orbit satellite and staring detector models, tracking task models, ...