1,275 karma · joined February 12, 2018
> But "fine" starts to feel slow when you need dense time resolution. Generating a month of ephemeris data at one-second intervals is 2.6 million propagations per satellite.
Ok, except SGP4 loses its accuracy over WAY shorter time frames than a month (think hours/days)
> Pass prediction over a ground station network might need sub-second precision across weeks.
a) sub-second ephemeris for antenna pointing is crazy overkill, and b) same comment about accuracy as above.
It adds to a pretty large body of literature around this subject, the gist of which is "risk is going up, but we don't really have a good way of estimating what that means in terms of actual collision rates".
[1] https://github.com/USNavalResearchLaboratory/TrackerComponen...
edit: thank you all for your travel suggestions, but this was a tongue-in-cheek way of trying to point out the absurdity of the OP's comment about DC not being the "real world".
Yes, a basic mistake. I'm not sure what you're getting at with your comment, but this is literally the kind of thing that should be caught very early on, probably just by updating a few parameters (or even just one) in the attitude control sim and observing the outputs.
If this claim is true (a big "if", admittedly), this is a breakdown in the kind of fundamental systems engineering that they teach to undergrads building cubesats.