Dynamical Characteristics of a Tethered Stabilized Satellite.
Dynamical Characteristics of a Tethered Stabilized Satellite.
This work presents a preliminary investigation of the stability characteristics of a tethered satellite attitude with respect to the local vertical. Other relevant topics analyzed are the influence of orbital eccentricity and tether oscillations on the satellite dynamics and identification of possible resonances. Parameters that affect the attitude control are the tether length, the offset between the satellite center of mass and the attachment point, and the ballast mass.
- University of Padua Italy
Free motion of a rigid body, resonances, Application models in control theory, Stabilization of systems by feedback, stability, gravity gradient attitude stabilization; linear control; stability analysis, tethered satellite attitude
Free motion of a rigid body, resonances, Application models in control theory, Stabilization of systems by feedback, stability, gravity gradient attitude stabilization; linear control; stability analysis, tethered satellite attitude
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