Based on STK and Matlab Satellite Formation's Configuration Design and Simulation

Chang Ping Dang; Yuan Wen Cai; Tian Le; Yi Bin Zhao; Chao Jun Xin

doi:10.4028/www.scientific.net/AMR.823.411

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HomeAdvanced Materials ResearchAdvanced Materials Research Vol. 823Based on STK and Matlab Satellite Formation's...

Based on STK and Matlab Satellite Formation's Configuration Design and Simulation

Abstract:

According to the structural characteristics of satellite formation, and using the kinematic equations which expressed as fly-around form, designed a model for satellite formation configuration, analysed the relationship between fly-around parameters and the orbital elements, designed a method that meets the mission requirements of the satellite formation configuration, formulated a corresponding operation flow chart, listed several typical satellite formations of simple configuration and complex configuration. Finally, according to the general process of configuration design, obtaioned a configuration based on the requirments, and with the help of software STK and Matlab performed a formation configuration simulation that considering collision avoidance verification and adjustment. The simulation results show that the formation configuration design process and design method are basically right.

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Periodical:

Advanced Materials Research (Volume 823)

Pages:

411-416

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.823.411

Citation:

Cite this paper

Online since:

October 2013

Authors:

Chang Ping Dang, Yuan Wen Cai, Tian Le, Yi Bin Zhao, Chao Jun Xin

Keywords:

Configuration Design, Satellite Formation, STK

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