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For Low Earth Orbit inputs of
r = np.array([-6478150,0,1200000]) v = np.array([0.0,-7844.111438052,0.0])
The checked calculation in from_state_vector() uses these comparisons:
from_state_vector()
abs(out.v - v) # 0.000113, 9.1e-13, 2.1e-5 abs(out.r - r) # 1.9e-9, 0.0982, 1.164e-9
With a hardcoded tolerance of 1e-4. The position y element exceeds that here.
This could be resolved by using relative error instead of absolute.
#21, #18, and #17 seem related.
The text was updated successfully, but these errors were encountered:
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For Low Earth Orbit inputs of
The checked calculation in
from_state_vector()
uses these comparisons:With a hardcoded tolerance of 1e-4. The position y element exceeds that here.
This could be resolved by using relative error instead of absolute.
#21, #18, and #17 seem related.
The text was updated successfully, but these errors were encountered: