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export eop_filename | ||
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# EOP Data | ||
# ============================ | ||
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""" | ||
NutationCorrections | ||
Container to hold the nutation corrections and celestial pole offsets associated to a | ||
given IERS model (e.g., 2000A) | ||
### Fields | ||
- `δX, δY`: Celestial pole offsets referred to the model IAU2000A (rad). | ||
- `δΔψ, δΔϵ`: Nutation corrections in longitude and obliquity (rad) | ||
### See also | ||
See also [`EOPData`](@ref). | ||
""" | ||
struct NutationCorrections{T} | ||
δX::Vector{T} | ||
δY::Vector{T} | ||
δΔψ::Vector{T} | ||
δΔϵ::Vector{T} | ||
end | ||
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function NutationCorrections(::Type{T}=Float64) where T | ||
return NutationCorrections(T[], T[], T[], T[]) | ||
end | ||
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""" | ||
EOPData{T} | ||
EOP Data container. Data is parameterised by time expressed in Terrestrial Time (TT) days. | ||
### Fields | ||
- `filename` : File where the EOP data are stored. | ||
- `days_UTC`: UTC days since J2000. | ||
- `days_TT` : TT days since J2000. | ||
- `UT1_TT`: UT1 minus TT offset, in seconds. | ||
- `LOD`: Length of day offset (s). | ||
- `xp, yp`: Polar motion with respect to the crust (rad). | ||
- `nut1996, nut2003, nut2006`: nutation and CIP corrections. | ||
""" | ||
mutable struct EOPData{T} | ||
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filename::String | ||
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days_UTC::Vector{T} | ||
days_TT::Vector{T} | ||
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UT1_TT::Vector{T} | ||
LOD::Vector{T} | ||
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xp::Vector{T} | ||
yp::Vector{T} | ||
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nut1996::NutationCorrections{T} | ||
nut2003::NutationCorrections{T} | ||
nut2010::NutationCorrections{T} | ||
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end | ||
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function EOPData(::Type{T}=Float64) where T | ||
return EOPData( | ||
"", T[], T[], T[], T[], T[], T[], | ||
NutationCorrections(T), NutationCorrections(T), NutationCorrections(T) | ||
) | ||
end | ||
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function Base.show(io::IO, eop::EOPData) | ||
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if isempty(eop.days_UTC) | ||
println(io, "EOPData()") | ||
else | ||
println( | ||
io, | ||
"EOPData(filename=\"$(eop.filename), \"beg=\"$(eop.days_UTC[1]) (UTC)\", "* | ||
"end=\"$(eop.days_UTC[end]) (UTC)\")" | ||
) | ||
end | ||
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end | ||
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""" | ||
set_nutation_corr!(eop::EOPData, m::IERSModel, nc::NutationCorrections) | ||
Set the nutation and cip corrections associated to the IERS model `m` to `nc`. | ||
""" | ||
set_nutation_corr!(eop::EOPData, ::IERS1996, nc::NutationCorrections) = eop.nut1996 = nc | ||
set_nutation_corr!(eop::EOPData, ::IERS2003, nc::NutationCorrections) = eop.nut2003 = nc | ||
set_nutation_corr!(eop::EOPData, ::IERS2010, nc::NutationCorrections) = eop.nut2010 = nc | ||
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""" | ||
eop_filename(eop::EOPData) | ||
Get the loaded Earth Orientation Parameters (EOP) filename. | ||
""" | ||
function eop_filename(eop::EOPData) | ||
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if isempty(eop.filename) | ||
throw(ErrorException("Unable to retrieve filename, no EOP data has been loaded.")) | ||
end | ||
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return eop.filename | ||
end | ||
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# Interpolators | ||
# ============================ | ||
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""" | ||
NutCorrectionsInterpolator | ||
Container to store the interpolators for the nutation corrections and celestial pole offsets | ||
associated to a given IERS model. | ||
### See also | ||
See also [`EOPInterpolator`](@ref) | ||
""" | ||
struct NutCorrectionsInterpolator{T <: AbstractInterpolationMethod} | ||
δX::T | ||
δY::T | ||
δΔψ::T | ||
δΔϵ::T | ||
end | ||
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function NutCorrectionsInterpolator(::Type{T}) where T | ||
NutCorrectionsInterpolator( | ||
_akima_init(T), _akima_init(T), _akima_init(T), _akima_init(T) | ||
) | ||
end | ||
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function NutCorrectionsInterpolator(days_tt, nc::NutationCorrections) | ||
NutCorrectionsInterpolator( | ||
InterpAkima(days_tt, nc.δX), | ||
InterpAkima(days_tt, nc.δY), | ||
InterpAkima(days_tt, nc.δΔψ), | ||
InterpAkima(days_tt, nc.δΔϵ) | ||
) | ||
end | ||
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""" | ||
EOPInterpolator | ||
Container to store the interpolators for the loaded EOP data. | ||
""" | ||
mutable struct EOPInterpolator{T <: AbstractInterpolationMethod} | ||
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init::Bool | ||
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xp::T | ||
yp::T | ||
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ut1_tt::T | ||
lod::T | ||
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nut1996::NutCorrectionsInterpolator{T} | ||
nut2003::NutCorrectionsInterpolator{T} | ||
nut2010::NutCorrectionsInterpolator{T} | ||
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end | ||
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function EOPInterpolator(::Type{T}=Float64) where T | ||
EOPInterpolator( | ||
false, | ||
_akima_init(T), _akima_init(T), _akima_init(T), _akima_init(T), | ||
NutCorrectionsInterpolator(T), | ||
NutCorrectionsInterpolator(T), | ||
NutCorrectionsInterpolator(T) | ||
) | ||
end | ||
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function Base.show(io::IO, i::EOPInterpolator) | ||
println(io, "EOPInterpolator(init=$(i.init))") | ||
end | ||
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# Function to initialise a dummy Akima interpolator | ||
_akima_init(::Type{T}) where T = InterpAkima([1, 2, 3, 4, 5, 6], zeros(T, 6)) | ||
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# IERS Constants | ||
# ============================ | ||
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""" | ||
IERS_EOP_DATA | ||
Earth Orientation Parameters Data. | ||
### See also | ||
See also [`EOPData`](@ref). | ||
""" | ||
const IERS_EOP_DATA = EOPData(); | ||
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""" | ||
IERS_EOP | ||
Earth Orientation Parameters (EOP) interpolators. | ||
### See also | ||
See also [`load_eop!`](@ref) and [`EOPInterpolator`](@ref). | ||
""" | ||
const IERS_EOP = EOPInterpolator(); |
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export eop_load_data! | ||
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""" | ||
eop_load_data!(filename, m::IERS2010) | ||
Initialise the Earth Orientation Parameters (EOP) from a dedicated JSMD `.eop.dat` file. | ||
!!! note | ||
Currently, only EOP data associated to the IAU2006/2000A precession-nutation model | ||
is supported. | ||
""" | ||
function eop_load_data!(filename, m::IERS2010) | ||
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# Set the EOP data | ||
eop_set_data!(filename, m) | ||
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# Initialise the interpolators | ||
IERS_EOP.init = true | ||
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# Set polar motion | ||
IERS_EOP.xp = InterpAkima(IERS_EOP_DATA.days_TT, IERS_EOP_DATA.xp) | ||
IERS_EOP.yp = InterpAkima(IERS_EOP_DATA.days_TT, IERS_EOP_DATA.yp) | ||
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IERS_EOP.lod = InterpAkima(IERS_EOP_DATA.days_TT, IERS_EOP_DATA.LOD) | ||
IERS_EOP.ut1_tt = InterpAkima(IERS_EOP_DATA.days_TT, IERS_EOP_DATA.UT1_TT) | ||
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# Set nutation correction interpolators | ||
# TODO: ensure these are set! | ||
# nci1996 = NutCorrectionsInterpolator(IERS_EOP_DATA.days_TT, IERS_EOP_DATA.nut1996) | ||
# nci2003 = NutCorrectionsInterpolator(IERS_EOP_DATA.days_TT, IERS_EOP_DATA.nut2003) | ||
nci2010 = NutCorrectionsInterpolator(IERS_EOP_DATA.days_TT, IERS_EOP_DATA.nut2010) | ||
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# IERS_EOP.nut1996 = nci1996 | ||
# IERS_EOP.nut2003 = nci2003 | ||
IERS_EOP.nut2010 = nci2010 | ||
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@info "EOP initialised from file `$(filename)`." | ||
nothing | ||
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end | ||
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""" | ||
eop_set_data!(filename, m::IERSModel) | ||
Set Earth Orientation Parameters (EOP) to be used for frames transformations from a JSMD | ||
`.eop.dat` file, given a reference model `m`. | ||
""" | ||
function eop_set_data!(filename, m::IERSModel) | ||
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oldfile = IERS_EOP_DATA.filename | ||
days_utc, days_tt, xp, yp, ut1_tt, lod, δX, δY, δΔψ, δΔϵ = eop_read_data(filename) | ||
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if (!isempty(IERS_EOP_DATA.days_UTC)) | ||
@warn "Existing EOP data from \'$(oldfile)\' will be overwritten by \'$(filename)\'." | ||
end | ||
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# Set data time stamps | ||
IERS_EOP_DATA.filename = filename | ||
IERS_EOP_DATA.days_UTC = days_utc | ||
IERS_EOP_DATA.days_TT = days_tt | ||
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# Set TT-to-UT1 offset and LOD | ||
IERS_EOP_DATA.UT1_TT = ut1_tt | ||
IERS_EOP_DATA.LOD = lod | ||
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# Set polar motion coordinates | ||
IERS_EOP_DATA.xp = xp | ||
IERS_EOP_DATA.yp = yp | ||
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# Set the nutation corrections | ||
nc = NutationCorrections(δX, δY, δΔψ, δΔϵ) | ||
set_nutation_corr!(IERS_EOP_DATA, m, nc) | ||
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# TODO: convert these corrections to those for the other models! | ||
nothing | ||
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end | ||
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""" | ||
eop_read_data(filename) | ||
Read Earth Orientation Parameters (EOP) from a dedicated JSMD `.eop.dat` file. | ||
!!! note | ||
JSMD's `.eop.dat` EOP files are meant to have a fixed structure to ease the | ||
retrieval of the relevant EOP data. | ||
""" | ||
function eop_read_data(filename) | ||
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if !endswith(filename, "eop.dat") | ||
throw( | ||
ArgumentError( | ||
"EOP reader support only '.eop.dat' files! Please prepare " * | ||
"the data with \'eop_parse_csv\' and retry." | ||
) | ||
) | ||
end | ||
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# Load the file | ||
data = readdlm(filename; header=false) | ||
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# Retrieve UT1-UTC | ||
Δut1 = @view(data[:, 4]) | ||
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# Convert UTC days to TT seconds | ||
days_utc = @view(data[:, 1]) | ||
days_tai = map(t->Tempo.utc2tai(Tempo.DJ2000, t)[2], days_utc) | ||
days_tt = days_tai .+ Tempo.OFFSET_TAI_TT/Tempo.DAY2SEC | ||
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# Compute UT1-TT, in seconds | ||
sec_ut1 = days_utc/Tempo.DAY2SEC + Δut1 | ||
ut1_tt = sec_ut1 - days_tt*Tempo.DAY2SEC | ||
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# Retrieve other quantities | ||
xp = @view(data[:, 2]) | ||
yp = @view(data[:, 3]) | ||
lod = @view(data[:, 5]) | ||
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δX = data[:, 6] | ||
δY = data[:, 7] | ||
δΔψ = data[:, 6] | ||
δΔϵ = data[:, 7] | ||
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return days_utc, days_tt, xp, yp, ut1_tt, lod, δX, δY, δΔψ, δΔϵ | ||
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end |
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