Amazingly enough, I've done it again -- I prompted Hunchbacked to pull down his latest video.
It seems he didn't even consider the effects of varying gravity with altitude on the attitude of a spacecraft. That's rather odd since it's the only thing with an influence on a satellite's attitude.
And I only had to cite the moon itself as evidence.
Quick work. I knew I should have D/L'd it.
Varying gravity affects attitude? I don't get it, but at least I'll admit it.
I know gravity varies with altitude, of course; Newton's law, inverse square, got it. But doesn't the satellite's axis of lowest MOI align with the primary's center of mass, regardless of altitude?
I traced his changing-satellite-CoG notion (and diagram) to a student research paper done by a Jacob Bean at Va Tech - truthfully, the paper is over my head, but it seems to be concerned with controlling a satellite's rotation by internally shifting the CoG. It seems to be in the undergrad-student-research-project stage at the moment, not a commonly used method as HB tries to put it across. Bean states, in fact, "
we are the first group to obtain experimental data, to the authors' knowledge, involving moving masses as a primary means of satellite attitude control." Experiments have been done on a NASA research plane and a spacecraft simulator, but not actually on an orbiting satellite as yet, AFAIK.
Have you heard anything about this, as an actual working control method?