Pages that link to "Item:Q330736"
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The following pages link to Nonlinear dynamic analysis of a three-body tethered satellite system with deployment/retrieval (Q330736):
Displaying 9 items.
- Nonlinear dynamics of a satellite with deployable solar panel arrays (Q873378) (← links)
- Dynamics of a flexible multi-tethered satellite formation in a halo orbit with uncertain parameters (Q2025562) (← 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)
- Vibration and elastic wave propagation in spatial flexible damping panel attached to four special springs (Q2204468) (← links)
- Optimal deployment of spin-stabilized tethered formations with continuous thrusters (Q2308142) (← links)
- An analytical control law of length rate for tethered satellite system (Q2399265) (← links)
- A brief analysis of artificial satellites solar panels deployment considering a nonlinear dynamic model (Q2679181) (← links)
- Three-dimensional optimal deployment of a tethered subsatellite with an elastic tether (Q3518540) (← links)
- Arbitrarily high-order energy-conserving methods for Hamiltonian problems with quadratic holonomic constraints (Q6617017) (← links)