Abstract
The quantum satellites in-orbit mainly perform scientific experiments of space-ground high speed quantum key distribution, quantum entanglement distribution and quantum teleportation. All the experiments mentioned above require accurate space-ground calibration, which accomplish attitude maneuver and alignment between optic axis of satellite payload and ground optical station. According to the pointing accuracy demand of quantum key distribution, the paper proposes an attitude guidance law with the quaternion algorithm, based on magnetometer and double-vector attitude determination algorithm and in-orbit satellite attitude pointing mode. The paper carries out the numerical simulation of attitude pointing precision between optic axis and ground station from the orbit determination error point of view. The results prove that the proposed algorithm of the attitude guidance law can provide accurate calibration and achieve the attitude stabilization pointing precisely.
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Xi, T. et al. (2020). A Method for Attitude Guidance Law Generation Based on High Precision Space-Ground Integrated Calibration. In: Xu, Z., Parizi, R., Hammoudeh, M., Loyola-González, O. (eds) Cyber Security Intelligence and Analytics. CSIA 2020. Advances in Intelligent Systems and Computing, vol 1146. Springer, Cham. https://doi.org/10.1007/978-3-030-43306-2_58
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DOI: https://doi.org/10.1007/978-3-030-43306-2_58
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