Pages that link to "Item:Q315446"
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The following pages link to Equilibrium configurations of the tethered three-body formation system and their nonlinear dynamics (Q315446):
Displaying 8 items.
- Exact mesh shape design of large cable-network antenna reflectors with flexible ring truss supports (Q318059) (← links)
- Nonlinear dynamic analysis of a three-body tethered satellite system with deployment/retrieval (Q330736) (← links)
- Formation reconfiguration in restricted three body problem (Q612407) (← links)
- Three-dimensional multi-tethered satellite formation with the elements moving along Lissajous curves (Q736963) (← links)
- Invariant shape solutions of the spinning three craft Coulomb tether problem (Q868502) (← 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)
- Coulomb spacecraft formation flying: equilibrium points, periodic orbits, and center manifolds (Q2116259) (← links)
- Arbitrarily high-order energy-conserving methods for Hamiltonian problems with quadratic holonomic constraints (Q6617017) (← links)
