Long-term dynamic modeling of tethered spacecraft using nodal position finite element method and symplectic integration (Q5964714)
From MaRDI portal
 | This is the item page for this Wikibase entity, intended for internal use and editing purposes. Please use this page instead for the normal view: Long-term dynamic modeling of tethered spacecraft using nodal position finite element method and symplectic integration |
scientific article; zbMATH DE number 6547696
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Long-term dynamic modeling of tethered spacecraft using nodal position finite element method and symplectic integration |
scientific article; zbMATH DE number 6547696 |
Statements
Long-term dynamic modeling of tethered spacecraft using nodal position finite element method and symplectic integration (English)
0 references
1 March 2016
0 references
tethered spacecraft
0 references
dynamics
0 references
elastic tether
0 references
nodal position finite element method
0 references
symplectic integration
0 references
satellite deorbit
0 references
0 references
0 references
0 references
0 references
0 references
