Pages that link to "Item:Q2070797"
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The following pages link to Analysis of the dynamics of the formation of a tether group of three nanosatellites taking into account their motion around the centers of mass (Q2070797):
Displaying 5 items.
- Nonlinear dynamic analysis of a three-body tethered satellite system with deployment/retrieval (Q330736) (← links)
- Three-dimensional multi-tethered satellite formation with the elements moving along Lissajous curves (Q736963) (← links)
- Dynamics of a flexible multi-tethered satellite formation in a halo orbit with uncertain parameters (Q2025562) (← links)
- Method of forming a triangular rotating tethered constellation of spacecraft using electromagnetic forces (Q2695146) (← links)
- Analysis of dynamics and control during the deployment of an annular tether group of spacecraft (Q6147214) (← links)