Pages that link to "Item:Q4513637"
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The following pages link to Dynamics of a space vehicle with elastic deploying tether (Q4513637):
Displaying 8 items.
- The effect of the elasticity of an orbital tether system on the oscillations of a satellite (Q370536) (← links)
- Dynamics of variable-length tethers with application to tethered satellite deployment (Q551139) (← links)
- De-spinning of tethered space target via partially invariable deployment with tension control (Q783509) (← links)
- Three-dimensional optimal deployment of a tethered subsatellite with an elastic tether (Q3518540) (← links)
- (Q5228525) (← links)
- On the dynamics of deployment of an orbital structure with elastic elements (Q5294499) (← links)
- Implicit algorithms for solving the Cauchy problem for the equations of the dynamics of mechanical systems (Q5318164) (← links)
- Long-term dynamic modeling of tethered spacecraft using nodal position finite element method and symplectic integration (Q5964714) (← links)