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KOMPSAT-2 AOCS Control Mode & Power Safe Mode Design
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 Title & Authors
KOMPSAT-2 AOCS Control Mode & Power Safe Mode Design
Rhee, Seung-Wu; Kim, Hak-Jung; Lee, Joo-Jin;
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KOMPSAT-2 is the second Korean earth observation satellite after KOMPSAT-l: the 1 meter GSD cartographic capability and planning to launch at the end of 2005 by ROKOT launch vehicle. The dedicated AOCS operational modes are designed for KOMPSAT-2 based on KOMPSAT-l experience All of AOCS operational modes requires gyro information. To compensate this drawback, Power Safe Mode is designed and implemented. Successfully AOCS on-board software is developed and extensively verified through a nonlinear simulation process. The simulation results of Power Safe Mode and Science Fine Submode are provided to demonstrate its functionality as well as its performance.育ﺖ⨀Ă䀠煥獣愠獵扨敡瀀ソソソソ꣘ﺖ⨀꣘ﺖ⨀ᄈ돀䃍ﺖ⨀塨�⨀ꢰﶖ⨀돐灕잖⨀灕잖⨀ㄶ〴㤰㐰㘴㐀
KOMPSAT-2;spacecraft;attitude & orbit control system;control mode;power safe mode;B-dot;
 Cited by
6시 저궤도 위성에서 B-dot 제어기 역할과 고장분석,이승우;김홍중;손준원;

한국항공우주학회지, 2013. vol.41. 3, pp.200-209 crossref(new window)
Roles of B-dot Controller and Failure Analysis for Dawn-dusk LEO Satellite, Journal of the Korean Society for Aeronautical & Space Sciences, 2013, 41, 3, 200  crossref(new windwow)
S.- W. Rhee, 2002, KOMPSAT -2 Subsystem Specification for the Attitude & Orbit Control Subsystem(KARI Internal Doc.)

MTI & ASE, 2002, KOMPSAT-2 Magnetic Sun Pointing Safehold Interim Report