Multi-Satellite Relative Navigation Scheme for Microsatellites Using Inter-Satellite Radio Frequency Measurements.

Shiming Mo, Xiaojun Jin, Chen Lin, Wei Zhang, Zhaobin Xu, Zhonghe Jin
Author Information
  1. Shiming Mo: School of Aeronautics and Astronautics, Zhejiang University, Hangzhou 310027, China. ORCID
  2. Xiaojun Jin: School of Aeronautics and Astronautics, Zhejiang University, Hangzhou 310027, China. ORCID
  3. Chen Lin: School of Aeronautics and Astronautics, Zhejiang University, Hangzhou 310027, China.
  4. Wei Zhang: School of Aeronautics and Astronautics, Zhejiang University, Hangzhou 310027, China.
  5. Zhaobin Xu: School of Aeronautics and Astronautics, Zhejiang University, Hangzhou 310027, China.
  6. Zhonghe Jin: School of Aeronautics and Astronautics, Zhejiang University, Hangzhou 310027, China.

Abstract

The inter-satellite relative navigation method-based on radio frequency (RF) range and angle measurements-offers good autonomy and high precision, and has been successfully applied to two-satellite formation missions. However, two main challenges occur when this method is applied to multi-microsatellite formations: (i) the implementation difficulty of the inter-satellite RF angle measurement increases significantly as the number of satellites increases; and (ii) there is no high-precision, scalable RF measurement scheme or corresponding multi-satellite relative navigation algorithm that supports multi-satellite formations. Thus, a novel multi-satellite relative navigation scheme based on inter-satellite RF range and angle measurements is proposed. The measurement layer requires only a small number of chief satellites, and a novel distributed multi-satellite range measurement scheme is adopted to meet the scalability requirement. An inter-satellite relative navigation algorithm for multi-satellite formations is also proposed. This algorithm achieves high-precision relative navigation by fusing the algorithm and measurement layers. Simulation results show that the proposed scheme requires only three chief satellites to perform inter-satellite angle measurements. Moreover, with the typical inter-satellite measurement accuracy and an inter-satellite distance of around 1 km, the proposed scheme achieves a multi-satellite relative navigation accuracy of ~30 cm, which is about the same as the relative navigation accuracy of two-satellite formations. Furthermore, decreasing the number of chief satellites only slightly degrades accuracy, thereby significantly reducing the implementation difficulty of multi-satellite RF angle measurements.

Keywords

Grants

  1. 62073289/National Natural Science Foundation of China
  2. 209C05004/Primary Research and Development Plan of Zhejiang Province

Word Cloud

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