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A Method for Attitude Guidance Law Generation Based on High Precision Space-Ground Integrated Calibration

  • Tao XiEmail author
  • Jiancheng Li
  • Jun Wei
  • Heng Wang
  • Junfeng Li
  • Shuang Chen
  • Dongmei Kuang
Conference paper
  • 17 Downloads
Part of the Advances in Intelligent Systems and Computing book series (AISC, volume 1146)

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.

Keywords

Quantum satellites Space-Ground integrated calibration experiment Attitude maneuver Attitude guidance law 

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Copyright information

© Springer Nature Switzerland AG 2020

Authors and Affiliations

  • Tao Xi
    • 1
    Email author
  • Jiancheng Li
    • 1
  • Jun Wei
    • 1
  • Heng Wang
    • 1
  • Junfeng Li
    • 1
  • Shuang Chen
    • 1
  • Dongmei Kuang
    • 1
  1. 1.State Key Laboratory of Astronautic DynamicsXi’anChina

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