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Error analysis of angle-only navigation methods based on on-orbit satellite observations

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Positioning errors increase linearly with relative observation distance, emphasizing distance's impact on accuracy.
Simulation results indicate optimal positioning accuracy within 1,000 km of satellite targets to minimize errors.
The least squares method is utilized to derive equations for geometric position calculations with three satellites.
Observational errors from stellar and satellite sources significantly affect positioning accuracy in navigation systems.

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This analysis explores positioning accuracy using satellite observations, indicating relative distance impacts errors.

Li et al. (2025) studied this question.

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