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Dynamics Modeling and Simulation of Korean Communication, Ocean, and Meteorology Satellite
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 Title & Authors
Dynamics Modeling and Simulation of Korean Communication, Ocean, and Meteorology Satellite
No, Tae-Soo; Lee, Sang-Uk; Kim, Sung-Ju;
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COMS(Communication, Oceanography, and Meteorology Satellite) is the first Korean multi-purpose satellite which is planned to be deployed at the altitude of geosynchronous orbit above the Korean peninsular. Noting that COMS is composed of the main BUS structure, two deployable solar panels, one yoke, five reactions wheels, COMS is treated as a collection of 9 bodies and its nonlinear equations of motion are obtained using the multi-body dynamics approach. Also, a computer program is developed to analyze the COMS motion during the various mission phase. Quite often, the equations of motion have to be derived repeatedly to reflect the fact that the spacecraft dynamics change as its configuration, and therefore its degree of freedom varies. However, the equations of motion and simulation software presented in this paper are general enough to represent the COMS dynamics of various configurations with a minimum change in input files. There is no need to derive the equations of motion repeatedly. To show the capability of the simulation program, the spacecraft motion during the solar array partial and full deployment has been simulated and the results are summarized in this paper.
Satellite attitude motion ; Multi-body dynamics ; Nonlinear Simulation ; Solar array deployment
 Cited by
수동형 전개힌지를 이용한 전개형 우주 구조물의 전개 동특성 해석,최영준;오현웅;최용훈;이경주;

한국군사과학기술학회지, 2008. vol.11. 3, pp.161-168

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