Pages that link to "Item:Q2004135"
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The following pages link to Coupled orbit-attitude dynamics of tethered-SPS (Q2004135):
Displaying 8 items.
- Out-of-plane librations of spinning tethered satellite systems (Q642334) (← links)
- De-spinning of tethered space target via partially invariable deployment with tension control (Q783509) (← links)
- Rigid-flexible coupling effect on attitude dynamics of electric solar wind sail (Q2219601) (← links)
- Collecting solar power by formation flying systems around a geostationary point (Q2313838) (← links)
- A way for accelerated calculation of spacecraft motion in an atmosphere with a tethered aerodynamic stabilizer (Q2961180) (← links)
- On spacial motions of an orbital tethered system (Q4605665) (← links)
- Dynamics and Control of Spinning Tethers for Rendezvous in Elliptic Orbits (Q5188400) (← links)
- Long-term dynamic modeling of tethered spacecraft using nodal position finite element method and symplectic integration (Q5964714) (← links)