A scaling procedure is developed to transfer verification scenarios for attitude control algorithms from the specific mission dimensions to the dimensions of ground-based hardware demonstrators. The definition of a dimensionless similarity variable ensures a similar load on control moment gyroscopes actuators in spite of different testbed characteristics such as moment of inertia, wheel angular momentum, and even CMG array architecture.
Scaled Verification Scenarios for Agile AOCS Testbeds
2018
Sonstige
Elektronische Ressource
Unbekannt
AOCS for Agile Scientific Spacecraft with Mini CMGs
British Library Conference Proceedings | 2000
|Agile AOCS Definition for an Optical Earth Observation Mission: LSPIM
British Library Conference Proceedings | 2000
|AIAA | 1981
|