講演名 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))
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抄録(和)
抄録(英) 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.
キーワード(和)
キーワード(英) Time Dissemination / Geostationary Satellite / Real-Time Orbit Estimation / Input Estimation Filter
資料番号 SAT2004-138
発行日

研究会情報
研究会 SAT
開催期間 2004/10/15(から1日開催)
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開催地(英)
テーマ(和)
テーマ(英)
委員長氏名(和)
委員長氏名(英)
副委員長氏名(和)
副委員長氏名(英)
幹事氏名(和)
幹事氏名(英)
幹事補佐氏名(和)
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講演論文情報詳細
申込み研究会 Satellite Telecommunications (SAT)
本文の言語 ENG
タイトル(和)
サブタイトル(和)
タイトル(英) 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))
サブタイトル(和)
キーワード(1)(和/英) / Time Dissemination
第 1 著者 氏名(和/英) / Bang-Yeop Kim
第 1 著者 所属(和/英)
Communication Satellite Systems Department, COMS Program Office Korea Aerospace Research Institute
発表年月日 2004/10/15
資料番号 SAT2004-138
巻番号(vol) vol.104
号番号(no) 352
ページ範囲 pp.-
ページ数 8
発行日