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    <identifier>10.57760/sciencedb.43455</identifier>
    <datestamp>2026-07-20T10:27:27Z</datestamp>
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<oai_dc:dc xmlns:oai_dc="http://www.openarchives.org/OAI/2.0/oai_dc/" xmlns:dc="http://purl.org/dc/elements/1.1/" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xsi:schemaLocation="http://www.openarchives.org/OAI/2.0/oai_dc/ http://www.openarchives.org/OAI/2.0/oai_dc.xsd">
  <dc:date>2026-07-20</dc:date>
  <dc:title>Research on Orbit Prediction Based on Multi-source Satellite Orbit Characteristics and Multi-head Attention Mechanism-LSTM Model</dc:title>
  <dc:identifier>doi:10.57760/sciencedb.43455</dc:identifier>
  <dc:language>en</dc:language>
  <dc:description>High-precision orbit prediction is critical for stable navigation system operation and space safety. To address the limitation of existing data-driven approaches that rely on single-satellite historical data and fail to fully exploit shared information among similar satellites, this paper proposes an orbit error correction model integrating multi-source orbital features with a multi-head attention mechanism-enhanced LSTM. Random forest regression and permutation importance analysis are employed to select SGP4 position errors, Q4 and Beta Angle as core input features, thereby mitigating redundant-feature interference. Unlike single-satellite modeling, the proposed method trains the model using historical data from multiple BeiDou satellites with similar orbital characteristics and applies it to error prediction and orbit correction for BeiDou-3M14. This strategy enables the model to capture satellite-specific error evolution and common orbital error patterns across similar satellites. Experimental results show that residual rates in the X, Y and Z directions are 0.24%, 0.16% and 0.20%, respectively, with root mean square errors of 1.17 m, 0.96 m and 0.75 m, outperforming Long Short-Term Memory(LSTM), Back Propagation Neural Network(BP) and Support Vector Machine(SVM) methods. Further experiments analyze the effects of training-satellite number, neural units and sampling interval on model performance, and verify its applicability to different prediction durations, space targets and GLONASS. The results demonstrate that multi-head attention mechanism-LSTM(MHALSTM) improves SGP4 orbit prediction error correction and supports high-precision space target prediction and space situational awareness. However, its performance remains constrained by orbital similarity, sample size and complex low-Earth-orbit perturbations, and its long-term stability in complex environments requires further verification.</dc:description>
  <dc:subject>Multi-Head Attention mechanism; multi-source satellite orbit; orbit prediction; space target; random forest </dc:subject>
  <dc:creator>Tao Yang</dc:creator>
  <dc:rights>PUBLIC</dc:rights>
  <dc:rights>https://creativecommons.org/licenses/by-nc-nd/4.0/</dc:rights>
  <dc:type>dataset</dc:type>
  <dc:publisher>Science Data Bank</dc:publisher>
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