Abstract
This paper analyzes the configuration parameter determination technology and accuracy analysis method of spacecraft flying around formation in long-term and close-range. In this paper, the high-precision orbit determination based on dual frequency GNSS (Global Navigation Satellite System) self positioning data and the formation configuration determination technology under the constraints of small amplitude and high-precision instantaneous translation are solved; the univariate linear regression data processing and high-precision configuration determination technology based on high-precision inter satellite relative measurement data are realized; the problem of rapid evaluation of configuration parameters is solved. The series of results studied in this paper better could support high-precision configuration parameter determination and rapid formation configuration evaluation under the condition of long-time formation flight of double satellites, and provide dynamic reliability guarantee for the space safety and the business application of formation spacecraft.
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Kai, D. et al. (2023). Determination Technology and Accuracy Analysis of Configuration Parameters of Ground System Dual Satellite Formation Based on Navigation Data. In: Yan, L., Duan, H., Deng, Y. (eds) Advances in Guidance, Navigation and Control. ICGNC 2022. Lecture Notes in Electrical Engineering, vol 845. Springer, Singapore. https://doi.org/10.1007/978-981-19-6613-2_2
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DOI: https://doi.org/10.1007/978-981-19-6613-2_2
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