The motion of a subsatellite containing a rotor rotating with constant angular velocity is considered. The subsatellite is tethered to a space shuttle which is moving with constant angular velocity in a central Newtonian field. Conditions for the existence of relative equilibria are given and their stability is discussed.
On relative equilibria of a tethered gyrostat in central Newtonian field
ZAMM. Zeitschrift für angewandte Mathematik und Mechanik ; 77 , 1,Suppl. ; S53-S54
1997
2 Seiten
Aufsatz (Zeitschrift)
Englisch
Rotationsfrequenz , Raumfähre , Luftfahrzeug , Befestigung , Bewegungsbahn , Seilerware , Fahrzeug , Geschwindigkeit , Flugkörper , Raum , Raumfahrzeug , Raumflugzeug , Satellit , Seil , Verkehrsmittel , Warenart , Zugmittel , Größe (physikalisch) , Energietransport , Drehzahl
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