Hello, I have a simulink model based on the spacecraft dynamics example here:
https://www.mathworks.com/help/aeroblks/analyzing-spacecraft-attitude-profiles-with-satellite-scenario.html#SpacecraftDynamicsCustomAttitudeExample-1
that by default outputs the satellite position at intervals of roughly 10s when not pointing at specific targets (i.e. is in a "point at Nadir" state).

Is it possible to increase the temporal granularity across the whole orbit, in order to have for example a largest time step of 0.5s, even when pointing at Nadir?
Thank youHello, I have a simulink model based on the spacecraft dynamics example here:
https://www.mathworks.com/help/aeroblks/analyzing-spacecraft-attitude-profiles-with-satellite-scenario.html#SpacecraftDynamicsCustomAttitudeExample-1
that by default outputs the satellite position at intervals of roughly 10s when not pointing at specific targets (i.e. is in a "point at Nadir" state).

Is it possible to increase the temporal granularity across the whole orbit, in order to have for example a largest time step of 0.5s, even when pointing at Nadir?
Thank you Hello, I have a simulink model based on the spacecraft dynamics example here:
https://www.mathworks.com/help/aeroblks/analyzing-spacecraft-attitude-profiles-with-satellite-scenario.html#SpacecraftDynamicsCustomAttitudeExample-1
that by default outputs the satellite position at intervals of roughly 10s when not pointing at specific targets (i.e. is in a "point at Nadir" state).

Is it possible to increase the temporal granularity across the whole orbit, in order to have for example a largest time step of 0.5s, even when pointing at Nadir?
Thank you time granularity, satellite simulation MATLAB Answers — New Questions

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