TY - GEN
T1 - Satellite orbit determinations with angle-only data using 0.6m optical wide-field telescope in KASI
AU - Choi, Jin
AU - Kim, Bang Yeop
AU - Yim, Hong Suh
AU - Chang, Heon Young
PY - 2009
Y1 - 2009
N2 - We observed 4 satellites (2 MEO, 1 GEO and 1 obsolete) using an optical observation system with a 0.6m wide-field telescope in KASI (Korean Astronomy and Space Science Institute). The optics has a f-ratio of 2.92 and is capable of viewing 4 square-degree fields at the prime focus. The mount system has a maximum speed of 10 degree/sec. Observations are carried out during 23 nights. A large parts of errors is caused by expose start time and end-point determination. For coordinate correction, we used WCS (World Coordinate System) solution with GSC 1.1 catalogue, and finally reduced the errors by 13 arc seconds. We found that an obsolete satellite has brightness variation which continues for 4 minutes in every 16 minutes. Gauss method for initial orbit determination was tested using angle-only data simulated by KODAS (KASI Orbit Determination and Analysis System). And also through differential correction using f & g series, initial orbit determination results are improved. For effective GEO satellites survey observation and initial orbit determination we try to find most suitable time span for initial orbit determination trough Gauss method with observation data. The result for time span from 20 to 40 minutes show good with some errors. From our optical observation, we confirmed that the precise orbit determination need optical telescope system with narrow FOV (field of view), efficient algorithm for reducing errors, more effective initial orbit determination software for optical observation and cooperation with other observation system like SLR(satellite laser ranging).
AB - We observed 4 satellites (2 MEO, 1 GEO and 1 obsolete) using an optical observation system with a 0.6m wide-field telescope in KASI (Korean Astronomy and Space Science Institute). The optics has a f-ratio of 2.92 and is capable of viewing 4 square-degree fields at the prime focus. The mount system has a maximum speed of 10 degree/sec. Observations are carried out during 23 nights. A large parts of errors is caused by expose start time and end-point determination. For coordinate correction, we used WCS (World Coordinate System) solution with GSC 1.1 catalogue, and finally reduced the errors by 13 arc seconds. We found that an obsolete satellite has brightness variation which continues for 4 minutes in every 16 minutes. Gauss method for initial orbit determination was tested using angle-only data simulated by KODAS (KASI Orbit Determination and Analysis System). And also through differential correction using f & g series, initial orbit determination results are improved. For effective GEO satellites survey observation and initial orbit determination we try to find most suitable time span for initial orbit determination trough Gauss method with observation data. The result for time span from 20 to 40 minutes show good with some errors. From our optical observation, we confirmed that the precise orbit determination need optical telescope system with narrow FOV (field of view), efficient algorithm for reducing errors, more effective initial orbit determination software for optical observation and cooperation with other observation system like SLR(satellite laser ranging).
UR - http://www.scopus.com/inward/record.url?scp=77953525381&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:77953525381
SN - 9781615679089
T3 - 60th International Astronautical Congress 2009, IAC 2009
SP - 1782
EP - 1790
BT - 60th International Astronautical Congress 2009, IAC 2009
T2 - 60th International Astronautical Congress 2009, IAC 2009
Y2 - 12 October 2009 through 16 October 2009
ER -