| Presentation | 2004/10/15 Real-Time Orbit Estimation Technique using Input Estimation Filter Algorithm for Geostationary Satellite(System Engineering III)(Joint Conference on Satellite Communications 2004(JC-SAT 2004)) Bang-Yeop Kim, Bong-Kyu Park, Sang-Cherl Lee, |
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| PDF Download Page | PDF download Page Link |
| Abstract(in Japanese) | (See Japanese page) |
| Abstract(in English) | We examined the applying of Input Estimation Filter (IEF) algorithm to the real-time orbit determination for a geostationary satellite. Generally, the Extended Kalman Filter (EKF) algorithm has been used to the real-time orbit determination in satellite operation. The EKF algorithm is good for the general non-linear estimation problem and robust to the geostationary orbit determination during the non-maneuvering period. But when the orbital maneuvers were occurred, the ordinary EKF shows some large errors. The IEF algorithm has been used to the missile for the tracking of maneuvering target. This algorithm assumes that the target can shows irregular maneuvering motion any time and configures a bank of filters. The filters in the bank generate many possible estimated statuses and compare to the EKF solution, and the best estimated status were adapted and updated finally. In this paper, we are going to show the simulation results of the real-time orbit estimation output using EKF only and with IEF algorithm. Through the comparing the results we could expect that the IEF algorithm can increase the estimation accuracy especially when the north-south stationkeeping maneuver. |
| Keyword(in Japanese) | (See Japanese page) |
| Keyword(in English) | Time Dissemination / Geostationary Satellite / Real-Time Orbit Estimation / Input Estimation Filter |
| Paper # | SAT2004-138 |
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| Conference Information | |
| Committee | SAT |
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| Conference Date | 2004/10/15(1days) |
| Place (in Japanese) | (See Japanese page) |
| Place (in English) | |
| Topics (in Japanese) | (See Japanese page) |
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| Paper Information | |
| Registration To | Satellite Telecommunications (SAT) |
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| Language | ENG |
| Title (in Japanese) | (See Japanese page) |
| Sub Title (in Japanese) | (See Japanese page) |
| Title (in English) | Real-Time Orbit Estimation Technique using Input Estimation Filter Algorithm for Geostationary Satellite(System Engineering III)(Joint Conference on Satellite Communications 2004(JC-SAT 2004)) |
| Sub Title (in English) | |
| Keyword(1) | Time Dissemination |
| Keyword(2) | Geostationary Satellite |
| Keyword(3) | Real-Time Orbit Estimation |
| Keyword(4) | Input Estimation Filter |
| 1st Author's Name | Bang-Yeop Kim |
| 1st Author's Affiliation | Communication Satellite Systems Department, COMS Program Office Korea Aerospace Research Institute() |
| 2nd Author's Name | Bong-Kyu Park |
| 2nd Author's Affiliation | Communication Satellite Systems Department, COMS Program Office Korea Aerospace Research Institute |
| 3rd Author's Name | Sang-Cherl Lee |
| 3rd Author's Affiliation | Communication Satellite Systems Department, COMS Program Office Korea Aerospace Research Institute |
| Date | 2004/10/15 |
| Paper # | SAT2004-138 |
| Volume (vol) | vol.104 |
| Number (no) | 352 |
| Page | pp.pp.- |
| #Pages | 8 |
| Date of Issue | |