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Closed-loop control of spacecraft formations with applications on SPHERES

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Academic year: 2021

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Figure

Figure  2-4:  Effect  of  fuel  use on  position  cost  for  a  circular  orbit.
Fig.  2-6:  Reconfiguration  maneuver  for  a  circular  orbit  using  absolute  geometry constraints
Fig.  2-8:  Reconfiguration  maneuver  for  an  elliptical  orbit  using  absolute  geometry constraints
Fig.  2-10:  Fuel  management  as  fuel  balancing  window  size e  is  adjusted.
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