2018
DOI: 10.1007/s11424-018-6096-1
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Observability Analysis and Navigation Algorithm for Distributed Satellites System Using Relative Range Measurements

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Cited by 4 publications
(3 citation statements)
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“…In the following lemma, we show that Θ i (s, a) remains bounded under certain conditions. Lemma 4.1 Consider the sequence {Θ i (s, a)} generated by (4). If there exist constants δ ≥ 1 ≥ δ ≥ 0 and γ ≥ 0, such that the following inequalities hold…”
Section: Iteration Process Analysismentioning
confidence: 99%
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“…In the following lemma, we show that Θ i (s, a) remains bounded under certain conditions. Lemma 4.1 Consider the sequence {Θ i (s, a)} generated by (4). If there exist constants δ ≥ 1 ≥ δ ≥ 0 and γ ≥ 0, such that the following inequalities hold…”
Section: Iteration Process Analysismentioning
confidence: 99%
“…The spacecraft autonomous navigation system aims to determine the orbit of the spacecraft using onboard measurement information without the support of ground-based tracking. It plays a critical role for the success of space missions, especially in the case that the failure occurs in the communication system toward the ground stations [1][2][3][4][5] . Many autonomous navigation schemes have been proposed, such as satellite stellar refraction navigation [6,7] , autonomous navigation using visible planets [8][9][10] and X-ray pulsar-based navigation (XNAV) [11][12][13][14] .…”
Section: Introductionmentioning
confidence: 99%
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