Pages that link to "Item:Q2011414"
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The following pages link to Control of the deployment of a tethered orbital system with a small load into a vertical position (Q2011414):
Displaying 7 items.
- A novel underactuated control scheme for deployment/retrieval of space tethered system (Q783427) (← links)
- De-spinning of tethered space target via partially invariable deployment with tension control (Q783509) (← links)
- 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) (← links)
- Quasi-optimal stabilization of oscillatory systems with many degrees of freedom (Q2171295) (← links)
- Method of forming a triangular rotating tethered constellation of spacecraft using electromagnetic forces (Q2695146) (← links)
- MATHEMATICAL SIMULATION OF A TETHERED SATELLITE SYSTEM MOTION WITH AN INFLATABLE SPHERICAL BALLOON DURING A SPACECRAFT ORBIT INJECTION (Q5042930) (← links)
- Arbitrarily high-order energy-conserving methods for Hamiltonian problems with quadratic holonomic constraints (Q6617017) (← links)
