-
As discussed during the meeting on 03-06-2016, one of the main developments that is needed for Tudat is the implementation of the propagation of different types of orbital elements/equations of motion…
-
I'm recently working on computing access to targets on Earth from a satellite. I found pyephem to be the best resource for doing so (from the programming perspective), but I have a question in regards…
-
current single-pass propagator is extremely inaccurate for gravity (decaying orbits even without atmospheric drag), need to implement a better state propagator for Newtonian objects as described in th…
-
I am comparing the results from satellite trackers (e.g. Gpredict, Orbitron) and pyephem results. The range is the same but the range_velocity is different. Any idea?
Box88 updated
9 years ago