Class | rad_short_income |
In: |
radiation/rad_short_income.f90
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Note that Japanese and English are described in parallel.
短波入射 (太陽入射) を計算します.
Calculate short wave (insolation) incoming radiation.
ShortIncoming : | 短波入射 (太陽入射) の計算 |
———— : | ———— |
ShortIncoming : | Calculate short wave (insolation) incoming radiation. |
Subroutine : | |||
xy_InAngle(0:imax-1, 1:jmax) : | real(DP), intent(out), optional
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DistFromStarScld : | real(DP), intent(out), optional
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xy_CosZet(0:imax-1, 1:jmax) : | real(DP), intent(out), optional
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DiurnalMeanFactor : | real(DP), intent(out), optional | ||
PlanetLonFromVE : | real(DP), intent(out), optional
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FlagOutput : | logical , intent(in ), optional |
短波入射 (太陽入射) を計算します.
Calculate short wave (insolation) incoming radiation.
subroutine RadShortIncome( xy_InAngle, DistFromStarScld, xy_CosZet, DiurnalMeanFactor, PlanetLonFromVE, FlagOutput ) ! ! 短波入射 (太陽入射) を計算します. ! ! Calculate short wave (insolation) incoming radiation. ! ! モジュール引用 ; USE statements ! ! 日付および時刻の取り扱い ! Date and time handler ! use dc_calendar, only: DCCalInquire, DCCalDateEvalSecOfDay ! ヒストリデータ出力 ! History data output ! use gtool_historyauto, only: HistoryAutoPut ! 宣言文 ; Declaration statements ! implicit none real(DP), intent(out), optional :: xy_InAngle (0:imax-1, 1:jmax) ! sec ( 入射角 ). ! sec ( Incident angle ) real(DP), intent(out), optional :: DistFromStarScld ! 軌道長半径でスケーリングした恒星からの距離 ! Distance from the star scaled ! by semimajor axis of the planet's orbit real(DP), intent(out), optional :: xy_CosZet(0:imax-1, 1:jmax) ! cos( 入射角 ) ! cos( Incident angle ) real(DP), intent(out), optional :: DiurnalMeanFactor real(DP), intent(out), optional :: PlanetLonFromVE ! 中心星を中心とする座標における春分点から測った惑星の経度 ! Longitude of the planet measured from the vernal equinox ! in the coordinate that the central star is located on ! the origin. logical , intent(in ), optional :: FlagOutput ! 作業変数 ! Work variables ! integer:: i ! 経度方向に回る DO ループ用作業変数 ! Work variables for DO loop in longitude integer:: j ! 緯度方向に回る DO ループ用作業変数 ! Work variables for DO loop in latitude real(DP):: SinDel ! 赤緯 ! Declination real(DP):: CosZet ! 入射角 ! Incidence angle real(DP):: AngleMaxLon ! 入射が最大となる緯度 real(DP):: HourAngle ! 時角 ! Hour angle real(DP):: ClockByDay ! 時刻を日で表記したもの (0.0 - 1.0) ! Clock expressed by day (0.0 - 1.0) real(DP) :: xy_InAngleLV (0:imax-1, 1:jmax) ! sec ( 入射角 ). ! sec ( Incident angle ) ! (local variable) real(DP) :: DistFromStarScldLV ! Distance between the central star and the planet ! (local variable) real(DP) :: xy_CosZetLV (0:imax-1, 1:jmax) ! cos( 入射角 ) ! cos( Incident angle ) ! (local variable) real(DP) :: PlanetLonFromVELV integer :: hour_in_a_day, min_in_a_hour real(DP) :: sec_in_a_min, sec_in_a_day ! 実行文 ; Executable statement ! ! 初期化確認 ! Initialization check ! if ( .not. rad_short_income_inited ) then call MessageNotify( 'E', module_name, 'This module has not been initialized.' ) end if ! Set flag for diurnally averaged insolation : This is temporary one. ! if ( present( DiurnalMeanFactor ) ) then if ( ( .not. FlagAnnualMean ) .and. FlagDiurnalMean ) then !!$ DiurnalMeanFactor = 1.0_DP / PI DiurnalMeanFactor = -1.0e100_DP else DiurnalMeanFactor = 1.0_DP end if end if ! 同期回転日射のフラグ ! Flag for synchronous rotation if ( .not. FlagRadSynchronous ) then ! 年, 日平均日射の計算 ! Calculate annual mean, daily mean insolation ! if ( FlagAnnualMean .and. FlagDiurnalMean ) then do i = 0, imax - 1 do j = 1, jmax xy_CosZetLV(i,j) = IncomAIns + IncomBIns * cos( y_Lat(j) )**2 if ( xy_CosZetLV(i,j) > 0.0_DP ) then xy_InAngleLV(i,j) = 1.0_DP / xy_CosZetLV(i,j) else xy_InAngleLV(i,j) = 0. end if end do end do DistFromStarScldLV = 1.0_DP SinDel = 0.0_DP PlanetLonFromVELV = 0.0_DP else if ( .not. FlagAnnualMean ) then ! Set sine of declination and distance between a planet and a central star ! scaled with semi-major axis ! if ( FlagPerpetual ) then SinDel = PerpSinDel DistFromStarScldLV = PerpDistFromStarScld else call ShortIncomCalcOrbParam( SinDel, DistFromStarScldLV, PlanetLonFromVELV ) if ( present( PlanetLonFromVE ) ) PlanetLonFromVE = PlanetLonFromVELV end if call DCCalInquire( hour_in_day = hour_in_a_day, min_in_hour = min_in_a_hour, sec_in_min = sec_in_a_min ) sec_in_a_day = hour_in_a_day * min_in_a_hour * sec_in_a_min if ( FlagSpecifySolDay ) then ! case with solar day which is different from sec_in_a_day (rotation ! period) ClockByDay = mod( TimeN / SolDay, 1.0_DP ) else ! case with solar day which is the same as sec_in_a_day (rotation ! period) ClockByDay = DCCalDateEvalSecOfDay( TimeN, date = InitialDate ) ClockByDay = ClockByDay / sec_in_a_day end if !!$ write( 6, * ) '###', TimeN, ClockByDay, mod( TimeN / sec_in_a_day, 1.0_DP ) !!$ write( 60, * ) TimeN, ClockByDay, mod( TimeN / sec_in_a_day, 1.0_DP ) !!$ call flush( 60 ) do i = 0, imax - 1 do j = 1, jmax if ( FlagDiurnalMean ) then HourAngle = 0.0_DP else HourAngle = ClockByDay * 2.0_DP * PI - PI + x_Lon(i) end if CosZet = sin( y_Lat(j) ) * SinDel + cos( y_Lat(j) ) * sqrt( 1.0_DP - SinDel**2 ) * cos( HourAngle ) xy_CosZetLV(i,j) = CosZet if ( CosZet > 0.0_DP ) then xy_InAngleLV(i,j) = 1.0_DP / CosZet else xy_InAngleLV(i,j) = 0. end if end do end do else ! 対応していない入射タイプ ! not implemented insolation type ! call MessageNotify( 'E', module_name, 'This type of insolation is not impremented' ) end if else ! 短波入射 (太陽入射) を計算します. ! 同期回転惑星を想定しており, ! 常に経度 90 度で最大入射, 経度 180-360 度で入射ゼロとなっています. ! ! Calculate short wave (insolation) incoming radiation. ! A planet with synchronized rotation are assumed. ! Incoming is max at latitude 90 deg., and zero between 180 and 360 deg. constantly. do i = 0, imax - 1 AngleMaxLon = - PI / 2.0_DP + x_Lon( i ) do j = 1, jmax CosZet = cos( y_Lat(j) ) * cos( AngleMaxLon ) xy_CosZetLV(i,j) = CosZet if ( CosZet > 0.0_DP ) then xy_InAngleLV(i,j) = 1.0_DP / CosZet else xy_InAngleLV(i,j) = 0.0_DP end if DistFromStarScldLV = 1.0_DP end do end do end if if ( present( xy_InAngle ) ) then xy_InAngle = xy_InAngleLV end if if ( present( xy_CosZet ) ) then xy_CosZet = xy_CosZetLV end if if ( present( DistFromStarScld ) ) then DistFromStarScld = DistFromStarScldLV end if ! ヒストリデータ出力 ! History data output ! if ( present( FlagOutput ) ) then if ( FlagOutput ) then call HistoryAutoPut( TimeN, 'Decl' , asin(SinDel)*180.0_DP/PI ) call HistoryAutoPut( TimeN, 'DistFromStarScld', DistFromStarScldLV ) call HistoryAutoPut( TimeN, 'PlanetLonFromVE' , PlanetLonFromVELV*180.0_DP/PI ) end if else call HistoryAutoPut( TimeN, 'Decl' , asin(SinDel)*180.0_DP/PI ) call HistoryAutoPut( TimeN, 'DistFromStarScld', DistFromStarScldLV ) call HistoryAutoPut( TimeN, 'PlanetLonFromVE' , PlanetLonFromVELV*180.0_DP/PI ) end if end subroutine RadShortIncome
Subroutine : |
rad_short_income モジュールの初期化を行います. NAMELIST#rad_short_income_nml の読み込みはこの手続きで行われます.
"rad_short_income" module is initialized. "NAMELIST#rad_short_income_nml" is loaded in this procedure.
This procedure input/output NAMELIST#rad_short_income_nml .
subroutine RadShortIncomeInit ! ! rad_short_income モジュールの初期化を行います. ! NAMELIST#rad_short_income_nml の読み込みはこの手続きで行われます. ! ! "rad_short_income" module is initialized. ! "NAMELIST#rad_short_income_nml" is loaded in this procedure. ! ! モジュール引用 ; USE statements ! ! 種別型パラメタ ! Kind type parameter ! use dc_types, only: STDOUT ! 標準出力の装置番号. Unit number of standard output ! ファイル入出力補助 ! File I/O support ! use dc_iounit, only: FileOpen ! ヒストリデータ出力 ! History data output ! use gtool_historyauto, only: HistoryAutoAddVariable ! 暦と日時の取り扱い ! Calendar and Date handler ! use dc_calendar, only: DC_CAL_DATE, DCCalDateInquire, DCCalDateCreate, DCCalDateDifference, DCCalConvertByUnit ! NAMELIST ファイル入力に関するユーティリティ ! Utilities for NAMELIST file input ! use namelist_util, only: namelist_filename, NmlutilMsg, NmlutilAryValid ! 宣言文 ; Declaration statements ! implicit none integer:: EpochYear, EpochMonth, EpochDay, EpochHour, EpochMin ! 元期日時 (年月日時分). ! "TimeAtEpoch" が負の場合にこちらが使用される. ! ! Date at epoch (year, month, day, hour, minute) ! These are used when "TimeAtEpoch" is negative. real(DP):: EpochSec ! 元期日時 (秒). ! "TimeAtEpoch" が負の場合にこちらが使用される. ! ! Date at epoch (second) ! These are used when "TimeAtEpoch" is negative. type(DC_CAL_DATE):: EpochDate ! 元期の日時 ! Date at epoch real(DP) :: PerpDelDeg ! Declination angle in degree used for perpetual experiment real(DP) :: SolDayValue character(TOKEN) :: SolDayUnit integer:: unit_nml ! NAMELIST ファイルオープン用装置番号. ! Unit number for NAMELIST file open integer:: iostat_nml ! NAMELIST 読み込み時の IOSTAT. ! IOSTAT of NAMELIST read logical :: FlagUseOfEpochDate character(TOKEN):: date_print ! NAMELIST 変数群 ! NAMELIST group name ! namelist /rad_short_income_nml/ FlagRadSynchronous, FlagAnnualMean, FlagDiurnalMean, FlagPerpetual, PerpDelDeg, PerpDistFromStarScld, EpsOrb, PerLonFromVE, LonFromVEAtEpoch, Eccentricity, TimeAtEpoch, EpochYear, EpochMonth, EpochDay, EpochHour, EpochMin, EpochSec, MaxItrEccAnomaly, ThreEccAnomalyError, IncomAIns, IncomBIns, IncomAZet, IncomBZet, FlagSpecifySolDay, SolDayValue, SolDayUnit ! ! デフォルト値については初期化手続 "rad_short_income#RadShortIncomeInit" ! のソースコードを参照のこと. ! ! Refer to source codes in the initialization procedure ! "rad_short_income#RadShortIncomeInit" for the default values. ! ! 実行文 ; Executable statement ! if ( rad_short_income_inited ) return ! デフォルト値の設定 ! Default values settings ! FlagRadSynchronous = .false. FlagAnnualMean = .true. FlagDiurnalMean = .true. FlagPerpetual = .false. !--- PerpDelDeg = 0.0_DP PerpDistFromStarScld = 1.0_DP !--- EpsOrb = 23.5_DP ! Earth-like value PerLonFromVE = 0.0_DP LonFromVEAtEpoch = 280.0_DP ! This value results in the fact that the planet ! is located at the position of vernal equinox ! at 80 days after calculation with the use of ! "360day" calendar. Eccentricity = 0.0_DP TimeAtEpoch = 0.0_DP EpochYear = -1 EpochMonth = -1 EpochDay = -1 EpochHour = -1 EpochMin = -1 EpochSec = -1.0_DP !--- ! Sample values for the Earth ! References: ! Duffett-Smith, P., Practical astronomy with your calculator Third Edition, ! Cambridge University Press, pp.185, 1988. ! !!$ EpsOrb = 23.44_DP ! Rika nenpyo (Chronological !!$ ! Scientific Tables 2010) !!$ PerLonFromVE = 102.768413_DP + 180.0_DP ! Duffett-Smith (1988), p.105 !!$ ! modified (plus 180 degrees) !!$ LonFromVEAtEpoch = 99.403308_DP + 180.0_DP ! Duffett-Smith (1988), p.105 !!$ ! modified (plus 180 degrees) !!$ Eccentricity = 0.016713_DP ! Duffett-Smith (1988), p.105 !!$ TimeAtEpoch = -1.0_DP ! EpochXXX written below are used !!$ ! because this is negative. !!$ EpochYear = 1990 ! Duffett-Smith (1988), p.105 !!$ EpochMonth = 1 !!$ EpochDay = 1 !!$ EpochHour = 0 !!$ EpochMin = 0 !!$ EpochSec = 0.0_DP !--- ! Sample values for Mars ! References: ! Allison, M., Geophys. Res. Lett., 24, 1967-1970, 1997. ! !!$ EpsOrb = 25.19_DP ! Allison (1997) !!$ PerLonFromVE = 250.98_DP ! Allison (1997) (modified) !!$ LonFromVEAtEpoch = -10.342_DP ! Arbitrarily set for clarity !!$ ! This results in Ls ~ 0 at Time = 0 !!$ Eccentricity = 0.0934_DP ! Allison (1997), value at epoch J2000 !!$ TimeAtEpoch = 0.0_DP ! Arbitrarily set for clarity !!$ EpochYear = -1 ! not used !!$ EpochMonth = -1 !!$ EpochDay = -1 !!$ EpochHour = -1 !!$ EpochMin = -1 !!$ EpochSec = -1.0_DP !--- MaxItrEccAnomaly = 20 ThreEccAnomalyError = 1e-6_DP IncomAIns = 0.127_DP ! see dcpam document for reference IncomBIns = 0.183_DP ! see dcpam document for reference IncomAZet = 0.410_DP ! see dcpam document for reference IncomBZet = 0.590_DP ! see dcpam document for reference FlagSpecifySolDay = .false. SolDayValue = 0.0_DP SolDayUnit = 'sec' ! NAMELIST の読み込み ! NAMELIST is input ! if ( trim(namelist_filename) /= '' ) then call FileOpen( unit_nml, namelist_filename, mode = 'r' ) ! (in) rewind( unit_nml ) read( unit_nml, nml = rad_short_income_nml, iostat = iostat_nml ) ! (out) close( unit_nml ) call NmlutilMsg( iostat_nml, module_name ) ! (in) end if if ( ( .not. FlagAnnualMean ) .and. FlagDiurnalMean ) then call MessageNotify( 'E', module_name, 'FlagDiurnalMean cannot be true if FlagAnnualMean is false.' ) end if PerpSinDel = sin( PerpDelDeg * PI / 180.0_DP ) FlagUseOfEpochDate = .false. if ( TimeAtEpoch < 0.0_DP ) then call DCCalDateCreate( year = EpochYear, month = EpochMonth, day = EpochDay, hour = EpochHour, min = EpochMin, sec = EpochSec, date = EpochDate ) ! (out) optional TimeAtEpoch = DCCalDateDifference( start_date = InitialDate, end_date = EpochDate ) FlagUseOfEpochDate = .true. end if SolDay = DCCalConvertByUnit( SolDayValue, SolDayUnit, 'sec' ) ! 保存用の変数の割り付け ! Allocate variables for saving ! ! ヒストリデータ出力のためのへの変数登録 ! Register of variables for history data output ! !!$ call HistoryAutoAddVariable( 'xxxxx' , & !!$ & (/ 'lon ', 'lat ', 'sig', 'time'/), & !!$ & 'xxxx', 'W m-2' ) call HistoryAutoAddVariable( 'ISR' , (/ 'lon ', 'lat ', 'time'/), 'incoming shortwave', 'W m-2' ) call HistoryAutoAddVariable( 'Decl' , (/ 'time'/), 'declination angle', 'degree' ) call HistoryAutoAddVariable( 'DistFromStarScld' , (/ 'time'/), 'distance between the central star and the planet', '1' ) call HistoryAutoAddVariable( 'PlanetLonFromVE' , (/ 'time'/), 'planetary longitude from the vernal equinox', 'degree' ) ! 印字 ; Print ! call MessageNotify( 'M', module_name, '----- Initialization Messages -----' ) call MessageNotify( 'M', module_name, 'ShortIncomming:' ) call MessageNotify( 'M', module_name, ' FlagRadSynchronous = %b', l = (/ FlagRadSynchronous /) ) call MessageNotify( 'M', module_name, ' FlagAnnualMean = %b', l = (/ FlagAnnualMean /) ) call MessageNotify( 'M', module_name, ' FlagDiurnalMean = %b', l = (/ FlagDiurnalMean /) ) call MessageNotify( 'M', module_name, ' FlagPerpetual = %b', l = (/ FlagPerpetual /) ) call MessageNotify( 'M', module_name, ' PerpDelDeg = %f', d = (/ PerpDelDeg /) ) call MessageNotify( 'M', module_name, ' PerpDistFromStarScld = %f', d = (/ PerpDistFromStarScld /) ) call MessageNotify( 'M', module_name, ' EpsOrb = %f', d = (/ EpsOrb /) ) call MessageNotify( 'M', module_name, ' PerLonFromVE = %f', d = (/ PerLonFromVE /) ) call MessageNotify( 'M', module_name, ' Eccentricity = %f', d = (/ Eccentricity /) ) if ( FlagUseOfEpochDate ) then call DCCalDateInquire( date_print, date = EpochDate ) call MessageNotify( 'M', module_name, ' EpochDate = %c', c1 = trim(date_print) ) end if call MessageNotify( 'M', module_name, ' TimeAtEpoch = %f', d = (/ TimeAtEpoch /) ) call MessageNotify( 'M', module_name, ' LonFromVEAtEpoch = %f', d = (/ LonFromVEAtEpoch /) ) call MessageNotify( 'M', module_name, ' MaxItrEccAnomaly = %d', i = (/ MaxItrEccAnomaly /) ) call MessageNotify( 'M', module_name, ' ThreEccAnomalyError = %f', d = (/ ThreEccAnomalyError /) ) call MessageNotify( 'M', module_name, ' IncomAIns = %f', d = (/ IncomAIns /) ) call MessageNotify( 'M', module_name, ' IncomBIns = %f', d = (/ IncomBIns /) ) call MessageNotify( 'M', module_name, ' IncomAZet = %f', d = (/ IncomAZet /) ) call MessageNotify( 'M', module_name, ' IncomBZet = %f', d = (/ IncomBZet /) ) call MessageNotify( 'M', module_name, ' FlagSpecifySolDay = %b', l = (/ FlagSpecifySolDay /) ) call MessageNotify( 'M', module_name, ' SolDay = %f', d = (/ SolDay /) ) call MessageNotify( 'M', module_name, '-- version = %c', c1 = trim(version) ) rad_short_income_inited = .true. end subroutine RadShortIncomeInit
Variable : | |||
FlagAnnualMean : | logical, save
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Variable : | |||
FlagDiurnalMean : | logical, save
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Variable : | |||
FlagPerpetual : | logical, save
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Variable : | |||
FlagRadSynchronous : | logical
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Variable : | |||
IncomAIns : | real(DP), save
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Variable : | |||
IncomAZet : | real(DP), save
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Variable : | |||
IncomBIns : | real(DP), save
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Variable : | |||
IncomBZet : | real(DP), save
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Variable : | |||
LonFromVEAtEpoch : | real(DP), save
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Variable : | |||
MaxItrEccAnomaly : | integer, save
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Variable : | |||
PerLonFromVE : | real(DP), save
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Variable : | |||
PerpDistFromStarScld : | real(DP), save
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Variable : | |||
PerpSinDel : | real(DP), save
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Subroutine : | |||
SinDel : | real(DP), intent(out)
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DistFromStarScld : | real(DP), intent(out)
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PlanetLonFromVE : | real(DP), intent(out)
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短波入射 (太陽入射) を計算します.
Calculate short wave (insolation) incoming radiation.
subroutine ShortIncomCalcOrbParam( SinDel, DistFromStarScld, PlanetLonFromVE ) ! ! 短波入射 (太陽入射) を計算します. ! ! Calculate short wave (insolation) incoming radiation. ! ! モジュール引用 ; USE statements ! ! 日付および時刻の取り扱い ! Date and time handler ! use dc_calendar, only: DCCalInquire, DCCalDateChkLeapYear ! 宣言文 ; Declaration statements ! implicit none real(DP), intent(out) :: SinDel ! 赤緯 ! Declination real(DP), intent(out) :: DistFromStarScld ! 軌道長半径でスケーリングした恒星からの距離 ! Distance from the star scaled ! by semimajor axis of the planet's orbit real(DP), intent(out) :: PlanetLonFromVE ! 中心星を中心とする座標における春分点から測った惑星の経度 ! Longitude of the planet measured from the vernal equinox ! in the coordinate that the central star is located on ! the origin. ! 作業変数 ! Work variables ! integer:: itr ! イテレーション方向に回る DO ループ用作業変数 ! Work variables for DO loop in iteration direction real(DP):: MeanAnomaly ! 平均近点角 ! Mean anomaly real(DP):: EccAnomaly ! 離心近点角 ! eccentric anomaly real(DP):: EccAnomalyError ! ニュートン法における離心近点角の誤差 ! error of eccentric anomaly in Newton method real(DP):: TrueAnomaly ! 真点離角 ! true anomaly integer :: hour_in_a_day, min_in_a_hour, day_in_a_year integer, pointer:: day_in_month_ptr(:) => null() real(DP) :: sec_in_a_min, sec_in_a_day, sec_in_a_year ! 実行文 ; Executable statement ! ! 初期化確認 ! Initialization check ! if ( .not. rad_short_income_inited ) then call MessageNotify( 'E', module_name, 'This module has not been initialized.' ) end if ! 季節変化, 日変化がある場合の計算 ! Calculate with seasonal change and diurnal change ! call DCCalInquire( day_in_month_ptr = day_in_month_ptr , hour_in_day = hour_in_a_day, min_in_hour = min_in_a_hour, sec_in_min = sec_in_a_min ) ! Add 1 to day_in_month_ptr(2) if it is leap year. ! if ( DCCalDateChkLeapYear( TimeN, InitialDate ) ) then day_in_month_ptr(2) = day_in_month_ptr(2) + 1 end if day_in_a_year = sum( day_in_month_ptr ) deallocate( day_in_month_ptr ) sec_in_a_day = hour_in_a_day * min_in_a_hour * sec_in_a_min sec_in_a_year = day_in_a_year * sec_in_a_day MeanAnomaly = 2.0_DP * PI * ( TimeN - TimeAtEpoch ) / sec_in_a_year + ( LonFromVEAtEpoch - PerLonFromVE ) * PI / 180.0_DP MeanAnomaly = mod( MeanAnomaly, 2.0_DP * PI ) ! ニュートン法を用いて平均近点角から離心近点角を求める. ! Calculate eccentric anomaly from mean anomaly by using Newton method. EccAnomaly = MeanAnomaly do itr = 1, MaxItrEccAnomaly EccAnomalyError = EccAnomaly - Eccentricity * sin(EccAnomaly) - MeanAnomaly if ( abs(EccAnomalyError) <= ThreEccAnomalyError ) exit EccAnomaly = EccAnomaly - EccAnomalyError / ( 1.0_DP - Eccentricity * cos(EccAnomaly) ) EccAnomaly = mod( EccAnomaly, 2.0 * PI ) end do if ( itr > MaxItrEccAnomaly ) then call MessageNotify( 'E', module_name, 'Calculation for eccentric anomaly does not converge.' ) end if DistFromStarScld = 1.0_DP - Eccentricity * cos( EccAnomaly ) TrueAnomaly = 2.0_DP * atan( sqrt( ( 1.0d0 + Eccentricity ) / ( 1.0d0 - Eccentricity ) ) * tan( EccAnomaly / 2.0_DP ) ) PlanetLonFromVE = TrueAnomaly + PerLonFromVE * PI / 180.0_DP PlanetLonFromVE = mod( PlanetLonFromVE, 2.0_DP * PI ) SinDel = sin( EpsOrb * PI / 180.0_DP ) * sin( PlanetLonFromVE ) ! code for debug !!$ write( 60, * ) TimeN/sec_in_a_day, DCCalDateChkLeapYear(TimeN,date=InitialDate), day_in_a_year !!$ write( 6, * ) TimeN/sec_in_a_day, DCCalDateChkLeapYear(TimeN,date=InitialDate), day_in_a_year !!$ call flush( 60 ) !!$ write( 60, * ) TimeN/sec_in_a_day, asin(SinDel)*180.0/PI, DistFromStarScld, PlanetLonFromVE*180.0_DP/PI !!$ write( 6, * ) TimeN/sec_in_a_day, asin(SinDel)*180.0/PI, DistFromStarScld, PlanetLonFromVE*180.0_DP/PI !!$ call flush( 60 ) end subroutine ShortIncomCalcOrbParam
Variable : | |||
ThreEccAnomalyError : | real(DP), save
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Constant : | |||
module_name = ‘rad_short_income‘ : | character(*), parameter
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Variable : | |||
rad_short_income_inited = .false. : | logical, save
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Constant : | |||
version = ’$Name: $’ // ’$Id: rad_short_income.f90,v 1.6 2013/05/25 06:33:57 yot Exp $’ : | character(*), parameter
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Variable : | |||
xy_InAngle(:,:) : | real(DP), allocatable, save
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