2008 Asia Simulation Conference - 7th International Conference on System Simulation and Scientific Computing 2008
DOI: 10.1109/asc-icsc.2008.4675554
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Dynamics simulation of deployment of solar panels on oblique spacecraft

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Cited by 7 publications
(10 citation statements)
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“…The Gini concordance is adopted in evaluating the severity of the fault caused by particular links. On the basis of (14) two ascending sequences are depicted as [19]…”
Section: Formulation Of Gini Concordancementioning
confidence: 99%
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“…The Gini concordance is adopted in evaluating the severity of the fault caused by particular links. On the basis of (14) two ascending sequences are depicted as [19]…”
Section: Formulation Of Gini Concordancementioning
confidence: 99%
“…Torsion springs are often chosen to drive the solar array and the locking spring is used to make the solar array fixed after deployment. The driving mechanism Inappropriate driving torque of the locking torsion spring 10 Fault of the motor 11 Fault of the transmission unit 12 Impact caused by particles in space 13 Vibration caused by clearances of hinges 14 Bad thermal characteristic of honeycomb materials in the hinges 1 ∼ 4 are noted as 1 ∼ 4 and the locking mechanism in the hinges 1 ∼ 4 are noted as 1 ∼ 4 . The CCLs meet the requirement of motion coordination and synchronization during deployment, which are organized as CCL 1 , CCL 2 , and CCL 3 in Figure 9(c).…”
Section: Fault Mode Of the Solar Arraymentioning
confidence: 99%
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