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Registered METHOD FOR FAST AND PRECISE ORBIT PROPOGATION INCLUDING MANEUVER

위치유지조정 이후 정지궤도 위성의 신속하고 정확한 궤도정보 이용
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Inventors
Hwang Yoola, Lee Byoung-Sun, Kim Jae Hoon, Lee Soo Jeon
Application No.
13334988 (2011.12.22)
Publication No.
20120166084 (2012.06.28)
Registration No.
8600676 (2013.12.03)
Country
UNITED STATES
Project Code
10MR1700, Study on Space Qualification of Ka band Payload and Application Technology for COMS, Do-Seob Ahn
Abstract
A flight dynamics subsystem (FDS), a velocity increment calculation module, and operational methods of the same are provided. A used fuel quantity actually used in a satellite is calculated, and a velocity increment is calculated using the calculated fuel quantity. Therefore, an orbit of the satellite may be estimated more accurately.
KSP Keywords
Velocity increment, flight dynamics
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Status Patent Country KIPRIS
Registered 매뉴버를 포함하는 빠르고 정확한 궤도 전파 방법 KOREA KIPRIS