2011
DOI: 10.1016/j.actaastro.2011.02.009
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Experimental study on dynamics and control of tethered satellite systems with climber

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Cited by 40 publications
(19 citation statements)
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“…Thus, the complete suppression of the librational motion of a TSS using only the climber motion has not been focused on in [22,24]. Instead, Kojima et al [24] derived optimal climber acceleration profiles to reduce the residual librational motion as much as possible for specific initial conditions, and studied their effectiveness numerically and experimentally.…”
Section: Introductionmentioning
confidence: 98%
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“…Thus, the complete suppression of the librational motion of a TSS using only the climber motion has not been focused on in [22,24]. Instead, Kojima et al [24] derived optimal climber acceleration profiles to reduce the residual librational motion as much as possible for specific initial conditions, and studied their effectiveness numerically and experimentally.…”
Section: Introductionmentioning
confidence: 98%
“…Thus, the complete suppression of the librational motion of a TSS using only the climber motion has not been focused on in [22,24]. Instead, Kojima et al [24] derived optimal climber acceleration profiles to reduce the residual librational motion as much as possible for specific initial conditions, and studied their effectiveness numerically and experimentally. The controllers in [20][21][22]24,26] showed good results, however, they are not always applicable to real situations Nomenclature a 1 ; a 2 ; a 3 ; a 4 weighting coefficients for mission-function control k 1 ; k 2 control gains L 0 ; L m initial and desired tether length between mother satellite and subsatellite L total tether length ðL ¼ L 1 þ L 2 Þ L 1 ; L 2 tether lengths between mother satellite and climber and between climber and subsatellite, respectively L m1 ; L m2 desired tether lengths between mother satellite and climber and between climber and subsatellite, respectively L s1 ; L s2 initial tether lengths between mother satellite and climber and between climber and subsatellite, respectively M F ; M F1 ; M F2 mission functions m 1 ; m 2 masses of climber and subsatellite, respectively N conversion factor to non-dimensional scale,…”
Section: Introductionmentioning
confidence: 98%
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