文章摘要
Yuan Dehu(袁德虎)* **,Sun Jun* **,Han Fei * **,Chen Yang* **,Chen Yun* **.[J].高技术通讯(英文),2020,26(2):188~195
GNSS autonomous navigation method for HEO spacecraft
  
DOI:doi:10.3772/j.issn.1006-6748.2020.02.008
中文关键词: 
英文关键词: global navigation satellite system (GNSS), high earth orbit (HEO), chaotic oscillator, autonomous navigation
基金项目:
Author NameAffiliation
Yuan Dehu(袁德虎)* ** (* Shanghai Aerospace Control Technology Institute, Shanghai 201109, P.R.China) (**Shanghai Key Laboratory of Space Intelligent Control Technology, Shanghai 201109, P.R.China) 
Sun Jun* ** (* Shanghai Aerospace Control Technology Institute, Shanghai 201109, P.R.China) (**Shanghai Key Laboratory of Space Intelligent Control Technology, Shanghai 201109, P.R.China) 
Han Fei * ** (* Shanghai Aerospace Control Technology Institute, Shanghai 201109, P.R.China) (**Shanghai Key Laboratory of Space Intelligent Control Technology, Shanghai 201109, P.R.China) 
Chen Yang* ** (* Shanghai Aerospace Control Technology Institute, Shanghai 201109, P.R.China) (**Shanghai Key Laboratory of Space Intelligent Control Technology, Shanghai 201109, P.R.China) 
Chen Yun* ** (* Shanghai Aerospace Control Technology Institute, Shanghai 201109, P.R.China) (**Shanghai Key Laboratory of Space Intelligent Control Technology, Shanghai 201109, P.R.China) 
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中文摘要:
      
英文摘要:
      For global navigation satellite system (GNSS) in the application of high earth orbit (HEO) determination, there are problems such as small number of visible satellites and weak signal magnitude. The transmitting and receiving errors of GNSS signal in the environment of HEO space are analyzed, and related compensating scheme is also proposed. Acquisition of GNSS signal is implemented by using weak signal acquisition technology based on Duffing. Precise tracking of weak GNSS signal is also realized by adopting dynamic detection and compensation technology based on Duffing chaotic oscillator. Simulation results show that, certain acquisition sensitivity and navigation precision can be reached, and the acquisition and tracking of weak GNSS signal can be realized by using the proposed technology, which provides good technology support for autonomous navigation of HEO and large elliptical spacecrafts.
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