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🐎 Force specialization in sv_ecef_to_ecef
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disberd committed Aug 15, 2023
1 parent 4f24b33 commit f05c93b
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2 changes: 1 addition & 1 deletion src/orbit/sv_ecef_to_ecef.jl
Original file line number Diff line number Diff line change
Expand Up @@ -25,7 +25,7 @@ Convert the orbit state vector `sv` from an ECEF frame to another ECEF frame. T
`args...` must match those of the function [`r_ecef_to_ecef`](@ref) **without** the rotation
representation.
"""
function sv_ecef_to_ecef(sv::OrbitStateVector, args...)
function sv_ecef_to_ecef(sv::OrbitStateVector, args::Vararg{Any, N}) where N
D = r_ecef_to_ecef(DCM, args...)

# Since both frames does not have a significant angular velocity between
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