sarclee
Mechanical
- Jan 14, 2022
- 105
During modeling assembly, always assume subsystems as point mass with MOI if the subsystem is large...
But why don't we model the subsystem in a simplified model (shell models)?
When we want to check for coupling issue, we then better to use reduced model for subsystems to be integrated with spacecraft?
But why don't we model the subsystem in a simplified model (shell models)?
When we want to check for coupling issue, we then better to use reduced model for subsystems to be integrated with spacecraft?