Detumbling Method for Uncontrolled Satellite Based on Eddy Currents
For the capture and removal of a large uncontrolled rotating satellite, a detumbling method based on the electromagnetic principle is developed and verified. A numerical method, which applies to arbitrary shapes and a nonuniform field, is used to calculate the eddy current torque of a rotating condu...
Gespeichert in:
Veröffentlicht in: | Journal of guidance, control, and dynamics control, and dynamics, 2020-08, Vol.43 (8), p.1444-1455 |
---|---|
Hauptverfasser: | , , , , |
Format: | Artikel |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
Schreiben Sie den ersten Kommentar!