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Satellite optical load reconnaissance probability calculation method based on ground target surface element equivalence

A ground target and probability calculation technology, applied in the field of aerospace reconnaissance, can solve the problems of missing reconnaissance probability calculation, the probability of missing reconnaissance satellite actual beam reconnaissance to the target area, etc., to reduce the difficulty of operation and use, reduce the difficulty of solving, improve The effect of solving speed

Active Publication Date: 2022-07-12
中国人民解放军32035部队
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  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0003] To deal with foreign spacecraft reconnaissance, it is mainly to judge the payload transit time of non-cooperative space reconnaissance satellites to the ground target area and the detection probability of the target during the payload transit period. The traditional detection probability calculation is directly based on the premise that the satellite reconnaissance beam detects the target. The most basic reconnaissance probability calculation is missing, that is, the probability that the actual beam of the reconnaissance satellite is reconnaissance to the target area is missing

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  • Satellite optical load reconnaissance probability calculation method based on ground target surface element equivalence
  • Satellite optical load reconnaissance probability calculation method based on ground target surface element equivalence
  • Satellite optical load reconnaissance probability calculation method based on ground target surface element equivalence

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Embodiment 1

[0082] See figure 1 , figure 1 A schematic flowchart of a method for calculating a satellite optical load reconnaissance probability based on the equivalent surface element of a ground target provided by an embodiment of the present invention, the method for calculating the reconnaissance probability includes the steps:

[0083] S1. Based on the latitude and longitude coordinates of the ground target active area, simplify the ground target active area into a rectangular area to obtain the ground target surface element equivalent area.

[0084]Specifically, the latitude and longitude coordinates of the ground target activity area are obtained, and the maximum and minimum values ​​of the longitude and latitude coordinates in the longitude and latitude coordinates and the maximum and minimum values ​​of the latitude coordinates are used as a rectangular area to obtain the equivalent area of ​​the ground target surface element.

[0085] See figure 2 , figure 2 An equivalent s...

Embodiment 2

[0208] On the basis of the first embodiment, this embodiment provides a satellite optical load reconnaissance probability calculation device based on the equivalent ground target surface element. The reconnaissance probability calculation device includes: a ground target surface equivalent module, a first relative position A relationship judgment module, a second relative position relationship judgment module and a reconnaissance probability calculation module.

[0209] Specifically, the ground target surface element equivalent module is used to simplify the ground target active area into a rectangular area based on the latitude and longitude coordinates of the ground target active area to obtain the ground target surface area equivalent area. The first relative position relationship judging module is used for judging the first relative position relationship between the equivalent area of ​​the ground target surface element and the maximum payload field of view of the optical i...

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Abstract

The invention relates to a satellite optical load reconnaissance probability calculation method and device based on ground target surface element equivalence, and the method comprises the steps: simplifying a ground target activity region into a rectangular region based on the latitude and longitude coordinates of the ground target activity region, and obtaining a ground target surface element equivalent region; judging a first relative position relation between the equivalent area of the ground target surface element and the maximum load view field range of the optical imaging satellite; on the basis of the first relative position relation, judging a second relative position relation between the equivalent area of the ground target surface element and the actual detection breadth of the optical load of the optical imaging satellite; and based on the first relative position relation or the second relative position relation, calculating the reconnaissance probability of the satellite optical load to the target area in combination with the first equivalent width of the equivalent area of the ground target surface element vertical to the flight path direction of the satellite, the maximum load view field range and the actual detection breadth of the optical load. The method solves the problem that a non-cooperative optical reconnaissance satellite is lack of ground target reconnaissance probability calculation.

Description

technical field [0001] The invention belongs to the field of aerospace reconnaissance, in particular to a method for calculating the reconnaissance probability of a satellite optical load based on the equivalent surface element of a ground target. Background technique [0002] Optical imaging reconnaissance is to carry out photographic reconnaissance on the ground from the spacecraft by installing cameras or cameras. Commonly used remote sensing devices include visible light cameras, television cameras, infrared cameras and multispectral cameras. The most important feature of optical imaging reconnaissance is the high ground resolution, at least better than 5m, and the current highest resolution can reach 0.1m. [0003] Responding to foreign spacecraft reconnaissance is mainly to judge the payload transit time of non-cooperative space reconnaissance satellites to the ground target area and the detection probability of the target within the payload transit period. The traditi...

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Application Information

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IPC IPC(8): G06F17/18G01S13/90G01S7/02
CPCG06F17/18G01S13/90G01S7/02
Inventor 钟卫军曹申艺何健邓小桐程熠王涵王玉姣
Owner 中国人民解放军32035部队