I know that for docking the ISS disables all attitude control.
Incorrect. ISS remains in attitude control during the docking approach. It's only after contact and capture that both ISS and shuttle goes into free drift. It's only after the orbiter docking ring has been retracted for hard docking that attitude control is resumed.Are you 100% sure about that, because it's disabled in order to prevent any accidental movements during the critical phase of docking, if it where to move the results could be catastrophic.
Thorton,
Any thoughts about adding an attitude hold function to the CMG of your ISS model? It would be most helpful for ISS models; 1A, 2A, and 3A where the shuttle flew an R-Bar approach.
Ben
Not necessarily. Gravity gradient torque makes it difficult (ie, propulsively expensive) to maintain an inertial attitude. In addition, rotating at a synchronous rate means that you can keep a constant visual attitude reference to the horizon.Why do they keep the station rotating throughout the docking? Wouldn't it be easier to just kill the rotation throughout the whole docking?