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Simulation analysis of impulse characteristics of space debris irradiated by multi-pulse laser
Author(s): Zhengguo Lin; Xing Jin; Hao Chang; Xiangyu You
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Paper Abstract

Cleaning space debris with laser is a hot topic in the field of space security research. Impulse characteristics are the basis of cleaning space debris with laser. In order to study the impulse characteristics of rotating irregular space debris irradiated by multi-pulse laser, the impulse calculation method of rotating space debris irradiated by multi-pulse laser is established based on the area matrix method. The calculation method of impulse and impulsive moment under multi-pulse irradiation is given. The calculation process of total impulse under multi-pulse irradiation is analyzed. With a typical non-planar space debris (cube) as example, the impulse characteristics of space debris irradiated by multi-pulse laser are simulated and analyzed. The effects of initial angular velocity, spot size and pulse frequency on impulse characteristics are investigated.

Paper Details

Date Published: 20 February 2018
PDF: 7 pages
Proc. SPIE 10697, Fourth Seminar on Novel Optoelectronic Detection Technology and Application, 1069755 (20 February 2018); doi: 10.1117/12.2307073
Show Author Affiliations
Zhengguo Lin, Aerospace Engineering Univ. (China)
Xing Jin, Aerospace Engineering Univ. (China)
Hao Chang, Aerospace Engineering Univ. (China)
Xiangyu You, Aerospace Engineering Univ. (China)


Published in SPIE Proceedings Vol. 10697:
Fourth Seminar on Novel Optoelectronic Detection Technology and Application
Weiqi Jin; Ye Li, Editor(s)

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