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Algorithms for spacecraft formation flying navigation based on wireless positioning system measurements

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Figure

Figure 2.1: (Left)Signal transmission between DBS and TRX. (Right) TRX’s signal arrives at antenna array.
Figure 2.2: DBS ID signal and TRX response signal in an IRT period.
Figure 2.3: Relative position vector between two spacecraft.
Figure 2.4: Illustration of signal transmission time delay
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