一种实现光学隐身的卫星构型设计

doi:10.3969/j.issn.1674-1579.2017.01.010

Abstract

Abstract: Abstract：At present, the detection and recognition of Geosynchronous orbit space target mainly depend on the optical monitoring system to receive the reflected light from the sun. In view of the principle of visible light reflection and the calculation model of visible light reflection characteristic of space object, the design strategy of optical stealth satellite is proposed. The satellite platform configuration, solar panels and hemispherical hood are designed. The whole star shape is simulated and analyzed. Finally the concept of distributed satellites is put forward. The results show that the optical cross section (OCS) peak of the configuration reaches 0.082 m2, which has high concealment and is not easy to be detected and identified by optical monitoring system.

Key words: Keywords：stealth technology, optical stealth, configuration design

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URL: http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/10.3969/j.issn.1674-1579.2017.01.010

http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/Y2017/V43/I1/61

References

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A Satellite Configuration Design for Optical Stealth

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