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Did you adjust the MRP feedback control gains to be sensible for this small inertia? If not, you'll have a crazy fast response that will be unstable with the discrete time steps. |
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Hi there,
I am trying a simulation in Basilisk framework about attitude control with RWs.
In particular I am testing that with a sufficiently light satellite (20kg more or less).
The model I am using in this case is 'Honeywell_HR16', testing a wide range of OmegaV and maxMom for the three RW. I am reporting here instead the settings for the control:
So nothing to do, control errors are very high and apparently there is no chance to set up a control with such small mass.
Using higher mass (as reported in all Basilisk examples, around 300kg...) it perfectly works, just tuning RW characteristics.
Anyone else has experienced such a problem and known a possible solution?
I can provide more details about the simulation if needed.
Regards,
PDM
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