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Multi-Satellite Relative Navigation Scheme for Microsatellites Using Inter-Satellite Radio Frequency Measurements.
Mo, Shiming; Jin, Xiaojun; Lin, Chen; Zhang, Wei; Xu, Zhaobin; Jin, Zhonghe.
Afiliação
  • Mo S; School of Aeronautics and Astronautics, Zhejiang University, Hangzhou 310027, China.
  • Jin X; Key Laboratory of Micro-Nano Satellite Research, Hangzhou 310027, China.
  • Lin C; School of Aeronautics and Astronautics, Zhejiang University, Hangzhou 310027, China.
  • Zhang W; Key Laboratory of Micro-Nano Satellite Research, Hangzhou 310027, China.
  • Xu Z; School of Aeronautics and Astronautics, Zhejiang University, Hangzhou 310027, China.
  • Jin Z; Key Laboratory of Micro-Nano Satellite Research, Hangzhou 310027, China.
Sensors (Basel) ; 21(11)2021 May 27.
Article em En | MEDLINE | ID: mdl-34071947
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.
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Texto completo: 1 Coleções: 01-internacional Base de dados: MEDLINE Idioma: En Revista: Sensors (Basel) Ano de publicação: 2021 Tipo de documento: Article País de afiliação: China

Texto completo: 1 Coleções: 01-internacional Base de dados: MEDLINE Idioma: En Revista: Sensors (Basel) Ano de publicação: 2021 Tipo de documento: Article País de afiliação: China