Orbit Determination Algorithm using DGPS for Low Earth Orbit Satellite (2002 Joint Conference on Satellite Communications (JC-SAT 2002)--衛星通信技術及び一般)
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概要
- 論文の詳細を見る
In this paper, we have proposed orbit determination algorithm using DGPS for Low Earth Orbit (LEO) satellite as alternative about conventional methods and developed DGPS environment for simulation. The conventional radar tracking or optical method has some problems (more station needed for low orbit satellite, high cost, low accuracy and dependence of operation). But our DGPS orbit determination method can solve these problems. We have considered almost effective perturbations (asymmetry gravitational force, Sun's gravity, Moon's gravity, Solar pressure, Air drag) on ECI coordinate and showed their effects graphically. Using Extended Kalman Filter we have made linear system model and estimated state variables. To test DGPS orbit determination virtually using this algorithm, we have simulated DGPS environment in space including most effects (GPS satellites arrangement, clock errors, ionosphere delay, etc.). From this, we could confirm good performance and possibility of our proposed algorithm.
- 社団法人電子情報通信学会の論文
- 2002-10-04
著者
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Kim Hakjung
School Of Materials Science And Engineering Seoul National University
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Sohn YoungHo
Seoul National University, Korea Aerospace Research Institute
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Kee ChangDon
Seoul National University, Korea Aerospace Research Institute
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Kim HakJung
Seoul National University, Korea Aerospace Research Institute
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Lee SangRyool
Seoul National University, Korea Aerospace Research Institute
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Kim Hakjung
Seoul National University Korea Aerospace Research Institute
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Kee Changdon
Seoul National University Korea Aerospace Research Institute
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Sohn Youngho
Seoul National University Korea Aerospace Research Institute
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Lee Sangryool
Seoul National University Korea Aerospace Research Institute
関連論文
- Orbit Determination Algorithm using DGPS for Low Earth Orbit Satellite (2002 Joint Conference on Satellite Communications (JC-SAT 2002)--衛星通信技術及び一般)
- Efficient Attitude Determination Using GPS Multiple Antennas : Geometrical Concept