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!MNH_LIC Copyright 2000-2022 CNRS, Meteo-France and Universite Paul Sabatier
!MNH_LIC This is part of the Meso-NH software governed by the CeCILL-C licence
!MNH_LIC version 1. See LICENSE, CeCILL-C_V1-en.txt and CeCILL-C_V1-fr.txt
!MNH_LIC for details. version 1.
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!-----------------------------------------------------------------
! #######################
SUBROUTINE INI_AIRCRAFT
! #######################
!
!
!!**** *INI_AIRCRAFT* - user initializes the aircraft flight path
!!
!! PURPOSE
!! -------
!
!
!!** METHOD
!! ------
!!
!! Must be defined (for each aircraft):
!! ---------------
!!
!! No default exist for these variables.
!! ************************************
!!
!! 1) the model in which the aircraft will evolve
!! if NOT initialized, the aircraft is NOT used.
!!
!! 2) the possibility to switch from a model to its dad or kid
!! 'FIX' : NMODEL used during the run
!! 'MOB' : best resolution model used. NMODEL=1 is used at the beginning
!!
!!
!! 3) the type of aircraft
!!
!! 'AIRCRA' for aircraft
!!
!! 4) the takeoff date and time
!!
!! 5) the number of flight path segments (SEG)
!!
!! 6) the (SEG ) duration of flight in the segments, in the flight order (sec.)
!!
!! 6bis) TAIRCRAFT%ALTDEF : flag to define the mode of initialisation of
!! aircraft altitude TRUE for pressure (corresponding to %SEGP)
!! or FALSE for Z (corresponding to %SEGZ)
!!
!! 7) the (SEG+1) latitudes of the segments ends, in the flight order
!! first point is take-off
!! last point is landing
!!
!! 8) the (SEG+1) longitudes of the segments ends, in the flight order
!!
!! 9) the (SEG+1) pressure (%SEGP) or Z (%SEGZ) of the segments ends, in the flight order
!!
!!
!!
!! Can be defined (for each aircraft):
!! --------------
!!
!!
!! 9) the time step for data storage.
!! default is 60s
!!
!! 10) the name or title describing the balloon (8 characters)
!! default is the balloon type (6 characters) + the balloon numbers (2 characters)
!!
!!
!! EXTERNAL
!! --------
!!
!! IMPLICIT ARGUMENTS
!! ------------------
!!
!! REFERENCE
!! ---------
!!
!! AUTHOR
!! ------
!! Valery Masson * Meteo-France *
!!
!! MODIFICATIONS
!! -------------
!! Original 15/05/2000
!! Sept2009, A. Boilley add initialisation of aircraft altitude by Z
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! P. Wautelet 06/2022: reorganize flyers
! --------------------------------------------------------------------------
!
!* 0. DECLARATIONS
! ------------
!
USE MODD_AIRCRAFT_BALLOON
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USE MODE_MSG
IMPLICIT NONE
!
!
!* 0.1 declarations of arguments
!
!
!-------------------------------------------------------------------------------
!
! 0.2 declaration of local variables
!
!
!----------------------------------------------------------------------------
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NAIRCRAFTS = 0
ALLOCATE( TAIRCRAFTS(NAIRCRAFTS) )
IF ( NAIRCRAFTS < 1 ) RETURN
!
!* 1. Aircraft number 1
! -----------------
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#if 0
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TAIRCRAFTS(1)%NMODEL = 0
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TAIRCRAFTS(1)%MODEL = 'FIX'
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TAIRCRAFTS(1)%TYPE = 'AIRCRA'
!
!* aircraft flight name
!
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TAIRCRAFTS(1)%TITLE = 'DIMO19A'
!
!* time step for storage
!
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TAIRCRAFTS(1)%TFLYER_TIME%XTSTEP = 60.
!
!* take-off date and time
!
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TAIRCRAFTS(1)%LAUNCH%nyear = 2007
TAIRCRAFTS(1)%LAUNCH%nmonth = 04
TAIRCRAFTS(1)%LAUNCH%nday = 19
TAIRCRAFTS(1)%LAUNCH%xtime = 32280.
!
!* number of flight segments
!
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TAIRCRAFTS(1)%SEG = 168
!
!* initalisation of flag for pressure (T) or Z(F) for aicraft altitude
!
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TAIRCRAFTS(1)%ALTDEF = .TRUE.
!
!* allocation of the arrays
!
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ALLOCATE(TAIRCRAFTS(1)%SEGTIME(TAIRCRAFTS(1)%SEG ))
ALLOCATE(TAIRCRAFTS(1)%SEGLAT (TAIRCRAFTS(1)%SEG+1))
ALLOCATE(TAIRCRAFTS(1)%SEGLON (TAIRCRAFTS(1)%SEG+1))
!
!* duration of the segments (seconds)
!
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TAIRCRAFTS(1)%SEGTIME = (/ 60, 60, 60, 60, 60, 60,&
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60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60 /)
!
!* latitudes of the segments ends (1st point is takeoff, last point is landing)
! (decimal degrees)
!
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TAIRCRAFTS(1)%SEGLAT = (/ 44.39971, 44.40095, 44.40040, 44.39919, 44.39657,&
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44.39339, 44.38749, 44.37916, 44.37464, 44.37021,&
44.37045, 44.37059, 44.37443, 44.37222, 44.35214,&
44.36092, 44.38175, 44.40122, 44.41992, 44.43539,&
44.45071, 44.46737, 44.48038, 44.47368, 44.46140,&
44.45519, 44.46365, 44.46959, 44.47475, 44.48028,&
44.47210, 44.46509, 44.46825, 44.47021, 44.48252,&
44.50106, 44.52266, 44.54233, 44.55776, 44.56624,&
44.57126, 44.57083, 44.57098, 44.57155, 44.56524,&
44.56006, 44.56914, 44.57413, 44.57368, 44.56907,&
44.56207, 44.55547, 44.54991, 44.54553, 44.54143,&
44.53734, 44.53293, 44.52783, 44.52403, 44.52920,&
44.54065, 44.54570, 44.54875, 44.55127, 44.55372,&
44.56859, 44.58518, 44.56456, 44.53939, 44.54009,&
44.56265, 44.58650, 44.60879, 44.61819, 44.61754,&
44.61660, 44.62217, 44.61920, 44.61041, 44.60369,&
44.60041, 44.60191, 44.60322, 44.58885, 44.56374,&
44.54355, 44.52951, 44.50729, 44.48498, 44.46095,&
44.43832, 44.42894, 44.41980, 44.40837, 44.38897,&
44.36689, 44.35023, 44.33820, 44.33409, 44.33662,&
44.33859, 44.33223, 44.32123, 44.32175, 44.32951,&
44.33953, 44.35040, 44.36167, 44.37196, 44.37869,&
44.38493, 44.39208, 44.40101, 44.40943, 44.42089,&
44.44113, 44.46887, 44.49583, 44.51708, 44.53618,&
44.54475, 44.55005, 44.55511, 44.56009, 44.56446,&
44.56590, 44.56728, 44.56972, 44.57093, 44.57225,&
44.57260, 44.57197, 44.57016, 44.56544, 44.55235,&
44.53552, 44.54387, 44.55054, 44.56146, 44.56070,&
44.54054, 44.52130, 44.50292, 44.48638, 44.47290,&
44.45529, 44.43734, 44.41889, 44.39770, 44.37671,&
44.35838, 44.35707, 44.36639, 44.37534, 44.37753,&
44.37753, 44.37986, 44.38700, 44.39457, 44.39753,&
44.40017, 44.40076, 44.39730, 44.39181, 44.39756,&
44.39935, 44.39868, 44.39727, 44.39696 /)
!
!* longitudes of the segments ends (1st point is takeoff, last point is landing)
! (decimal degrees)
!
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TAIRCRAFTS(1)%SEGLON = (/0.75561, 0.73090, 0.70157, 0.66896, 0.63468,&
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0.60107, 0.56909, 0.53738, 0.50474, 0.47315,&
0.44092, 0.40665, 0.37725, 0.35171, 0.33016,&
0.31340, 0.29638, 0.27594, 0.25293, 0.22663,&
0.19920, 0.17395, 0.15872, 0.17700, 0.19870,&
0.21796, 0.20584, 0.18416, 0.16200, 0.16042,&
0.18704, 0.20952, 0.19838, 0.17702, 0.15936,&
0.13843, 0.11309, 0.08309, 0.04845, 0.00948,&
-0.03097,-0.07187,-0.11372,-0.15500,-0.19571,&
-0.23476,-0.26490,-0.29027,-0.31521,-0.33867,&
-0.36085,-0.38222,-0.40476,-0.42847,-0.45149,&
-0.47413,-0.49675,-0.51926,-0.54853,-0.58352,&
-0.61936,-0.65967,-0.70151,-0.74369,-0.78626,&
-0.82035,-0.82679,-0.81080,-0.80093,-0.81855,&
-0.83421,-0.84543,-0.85947,-0.88928,-0.92270,&
-0.95642,-0.98774,-1.01802,-1.05282,-1.08807,&
-1.12390,-1.15847,-1.19287,-1.22142,-1.24147,&
-1.26289,-1.28825,-1.28869,-1.27067,-1.25984,&
-1.25447,-1.22868,-1.19892,-1.16909,-1.14878,&
-1.13185,-1.10636,-1.07398,-1.03438,-1.00077,&
-0.97309,-0.94428,-0.91011,-0.87900,-0.85405,&
-0.83235,-0.81217,-0.79231,-0.77125,-0.74612,&
-0.71985,-0.69334,-0.66698,-0.64049,-0.61627,&
-0.59738,-0.58007,-0.55652,-0.52248,-0.48603,&
-0.44405,-0.39964,-0.35780,-0.32620,-0.29894,&
-0.27061,-0.24144,-0.21229,-0.18267,-0.15256,&
-0.12223,-0.09116,-0.05346,-0.00969, 0.03348,&
0.07270, 0.07334, 0.03393, 0.00021, 0.01935,&
0.05295, 0.08646, 0.11585, 0.14321, 0.17288,&
0.20083, 0.22825, 0.25199, 0.27166, 0.29386,&
0.31926, 0.35232, 0.38587, 0.41831, 0.45384,&
0.49099, 0.52731, 0.56261, 0.59614, 0.63308,&
0.67001, 0.70471, 0.73740, 0.76830, 0.76841,&
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0.75848, 0.76209, 0.76315, 0.76335 /)
!
!* pressure of the segments ends (1st point is takeoff, last point is landing)
! (pascals)
!
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IF (TAIRCRAFTS(1)%ALTDEF) THEN
ALLOCATE(TAIRCRAFTS(1)%SEGP (TAIRCRAFTS(1)%SEG+1))
TAIRCRAFTS(1)%SEGP = 100. * (/1003.6, 990.8, 988.1, 988.5, 989.3,&
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988.9, 989.6, 989.9, 990.3, 989.2,&
990.8, 993.9, 987.7, 987.2, 992.0,&
995.2, 993.9, 994.0, 994.3, 993.9,&
993.9, 992.6, 981.6, 968.0, 954.6,&
942.5, 929.8, 917.8, 904.2, 891.8,&
879.5, 867.9, 857.0, 846.5, 840.0,&
844.9, 857.8, 873.5, 889.7, 905.3,&
921.5, 937.8, 953.9, 963.7, 978.8,&
993.0, 984.1, 970.4, 955.6, 943.1,&
930.3, 916.8, 904.4, 891.6, 878.6,&
866.2, 854.3, 846.2, 851.2, 863.0,&
878.3, 895.0, 912.3, 929.7, 944.7,&
959.2, 967.2, 977.6, 981.9, 981.1,&
982.1, 981.9, 984.4, 984.2, 983.6,&
982.1, 978.6, 980.5, 982.1, 983.1,&
984.2, 984.5, 983.6, 996.0,1003.8,&
1004.2,1001.4,1000.5,1002.3,1005.9,&
1000.9, 992.8, 989.7, 987.1, 985.1,&
984.3, 982.4, 986.7, 999.1, 994.8,&
984.1, 985.1, 997.0, 988.2, 975.0,&
963.0, 949.0, 937.4, 925.3, 912.6,&
898.8, 886.1, 873.6, 860.8, 848.3,&
850.2, 863.4, 880.2, 898.0, 916.3,&
932.8, 949.7, 959.7, 947.5, 933.3,&
920.8, 907.4, 894.0, 881.4, 869.0,&
858.0, 848.9, 852.2, 863.2, 880.0,&
895.3, 909.6, 926.1, 942.0, 958.6,&
977.3, 993.0, 995.6, 995.0, 993.0,&
996.2, 995.1, 994.2, 993.4, 993.6,&
992.0, 991.3, 993.2, 991.6, 993.1,&
992.7, 992.0, 992.0, 989.4, 991.2,&
989.5, 981.8, 977.8, 983.3,1001.9,&
1007.0,1006.8,1006.8, 1006.8 /)
ELSE
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ALLOCATE(TAIRCRAFTS(1)%SEGZ (TAIRCRAFTS(1)%SEG+1))
TAIRCRAFTS(1)%SEGZ = (/8000,8000,8000,8000,8000,&
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8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
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8000,8000,8000,8000 /)
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IF ( NAIRCRAFTS < 2 ) RETURN
#else
CALL PRINT_MSG( NVERB_FATAL, 'GEN', 'INI_AIRCRAFT', 'aircraft characteristics are commented' )
#endif
!----------------------------------------------------------------------------
!
!* 1. Aircraft number 2
! -----------------
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#if 0
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TAIRCRAFTS(2)%NMODEL = 0
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TAIRCRAFTS(2)%MODEL = 'FIX'
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TAIRCRAFTS(2)%TYPE = 'AIRCRA'
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TAIRCRAFTS(2)%TITLE = 'DIMO19B'
!
!* time step for storage
!
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TAIRCRAFTS(2)%TFLYER_TIME%XTSTEP = 60.
!
!* take-off date and time
!
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TAIRCRAFTS(2)%LAUNCH%nyear = 2007
TAIRCRAFTS(2)%LAUNCH%nmonth = 04
TAIRCRAFTS(2)%LAUNCH%nday = 19
TAIRCRAFTS(2)%LAUNCH%xtime = 48060.
!
!* number of flight segments
!
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TAIRCRAFTS(2)%SEG = 198
!
!* initalisation of flag for pressure (T) or Z(F) for aicraft altitude
!
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TAIRCRAFTS(2)%ALTDEF = .TRUE.
!
!* allocation of the arrays
!
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ALLOCATE(TAIRCRAFTS(2)%SEGTIME(TAIRCRAFTS(2)%SEG ))
ALLOCATE(TAIRCRAFTS(2)%SEGLAT (TAIRCRAFTS(2)%SEG+1))
ALLOCATE(TAIRCRAFTS(2)%SEGLON (TAIRCRAFTS(2)%SEG+1))
!
!* duration of the segments (seconds)
!
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TAIRCRAFTS(2)%SEGTIME = (/60, 60, 60, 60, 60, 60,&
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60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60,&
60, 60, 60, 60, 60, 60 /)
!
!* latitudes of the segments ends (1st point is takeoff, last point is landing)
! (decimal degrees)
!
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TAIRCRAFTS(2)%SEGLAT = (/ 44.39819, 44.39967, 44.40104, 44.40074, 44.40085,&
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44.39843, 44.39619, 44.39141, 44.38353, 44.37732,&
44.37508, 44.37609, 44.37377, 44.36764, 44.36083,&
44.35442, 44.37187, 44.39327, 44.41394, 44.43280,&
44.44887, 44.46759, 44.47026, 44.45759, 44.46716,&
44.48098, 44.49223, 44.48031, 44.46436, 44.46050,&
44.46611, 44.47339, 44.47535, 44.46444, 44.46467,&
44.47678, 44.49333, 44.50428, 44.51275, 44.52244,&
44.53453, 44.54696, 44.55673, 44.56092, 44.56132,&
44.56116, 44.56225, 44.56290, 44.56055, 44.55233,&
44.54409, 44.53433, 44.52137, 44.50897, 44.49627,&
44.48420, 44.47599, 44.46897, 44.46110, 44.45206,&
44.44454, 44.43702, 44.42862, 44.41992, 44.40707,&
44.38769, 44.36858, 44.34945, 44.32974, 44.30938,&
44.28888, 44.26943, 44.27339, 44.29464, 44.32345,&
44.35428, 44.38620, 44.41810, 44.43924, 44.42371,&
44.40729, 44.39663, 44.39174, 44.38035, 44.35685,&
44.35082, 44.37277, 44.37210, 44.37059, 44.37076,&
44.36948, 44.35924, 44.34744, 44.34207, 44.33859,&
44.33485, 44.32219, 44.30517, 44.28314, 44.25674,&
44.23110, 44.20517, 44.18849, 44.18723, 44.18804,&
44.18820, 44.18341, 44.16808, 44.14988, 44.12651,&
44.09887, 44.10007, 44.13022, 44.15963, 44.16313,&
44.14156, 44.11520, 44.08806, 44.06374, 44.05124,&
44.04458, 44.04106, 44.04035, 44.04010, 44.03897,&
44.03530, 44.03939, 44.05114, 44.06269, 44.07460,&
44.08650, 44.09131, 44.08050, 44.09213, 44.10666,&
44.12659, 44.14738, 44.16590, 44.18314, 44.19906,&
44.21885, 44.24219, 44.26652, 44.29116, 44.31433,&
44.33735, 44.36057, 44.37947, 44.39634, 44.41202,&
44.42718, 44.44310, 44.45702, 44.46577, 44.47367,&
44.47522, 44.48508, 44.49589, 44.50652, 44.51467,&
44.52342, 44.53589, 44.54841, 44.55751, 44.55326,&
44.54398, 44.53334, 44.52054, 44.50654, 44.49421,&
44.48487, 44.47112, 44.45230, 44.43285, 44.41224,&
44.39065, 44.36929, 44.35484, 44.35927, 44.36936,&
44.37609, 44.37666, 44.37590, 44.38037, 44.38779,&
44.39413, 44.39740, 44.40002, 44.40032, 44.39755,&
44.39226, 44.39494, 44.39910, 44.39862, 44.39719,&
44.39691, 44.39692, 44.39689, 44.39694 /)
!
!* longitudes of the segments ends (1st point is takeoff, last point is landing)
! (decimal degrees)
!
WAUTELET Philippe
committed
TAIRCRAFTS(2)%SEGLON = (/0.76323, 0.75549, 0.73212, 0.70405, 0.67289,&
478
479
480
481
482
483
484
485
486
487
488
489
490
491
492
493
494
495
496
497
498
499
500
501
502
503
504
505
506
507
508
509
510
511
512
513
514
515
516
517
518
519
520
0.64082, 0.60831, 0.57717, 0.54697, 0.51578,&
0.48245, 0.45056, 0.41783, 0.38851, 0.36046,&
0.32828, 0.30353, 0.28176, 0.25886, 0.23647,&
0.21031, 0.18783, 0.19138, 0.20574, 0.19556,&
0.17902, 0.17207, 0.18561, 0.20057, 0.21096,&
0.19209, 0.17406, 0.18880, 0.21157, 0.20492,&
0.17724, 0.14803, 0.11416, 0.07884, 0.04294,&
0.00754,-0.02836,-0.06645,-0.10613,-0.14594,&
-0.18382,-0.21191,-0.23806,-0.26153,-0.28229,&
-0.30235,-0.32461,-0.35502,-0.38888,-0.42649,&
-0.46658,-0.49951,-0.52354,-0.54620,-0.56911,&
-0.59210,-0.61530,-0.63781,-0.66103,-0.68000,&
-0.68664,-0.68859,-0.68904,-0.68633,-0.68257,&
-0.67785,-0.67856,-0.68504,-0.67421,-0.65909,&
-0.64292,-0.62468,-0.60554,-0.60962,-0.64284,&
-0.68049,-0.72153,-0.76308,-0.79993,-0.82295,&
-0.80244,-0.79925,-0.83586,-0.87284,-0.90717,&
-0.93954,-0.96673,-0.99345,-1.02688,-1.06013,&
-1.09311,-1.12010,-1.14430,-1.15772,-1.15729,&
-1.15461,-1.15633,-1.17298,-1.19786,-1.22215,&
-1.24575,-1.26738,-1.27606,-1.27726,-1.28392,&
-1.29406,-1.29028,-1.29255,-1.28781,-1.27630,&
-1.29478,-1.30461,-1.31179,-1.30894,-1.28378,&
-1.25748,-1.23181,-1.20656,-1.17989,-1.15381,&
-1.12789,-1.10402,-1.08189,-1.05854,-1.03571,&
-1.01321,-0.98957,-0.98981,-0.98826,-0.96629,&
-0.94082,-0.91032,-0.87556,-0.83647,-0.79522,&
-0.75987,-0.73047,-0.70212,-0.67419,-0.64559,&
-0.61580,-0.58662,-0.56599,-0.55283,-0.53912,&
-0.52493,-0.51192,-0.49392,-0.47041,-0.45111,&
-0.43705,-0.41091,-0.38491,-0.35776,-0.32809,&
-0.29403,-0.25181,-0.20625,-0.15899,-0.11076,&
-0.06454,-0.01989, 0.02357, 0.06550, 0.10835,&
0.15086, 0.18573, 0.21197, 0.23662, 0.25944,&
0.28144, 0.30338, 0.32757, 0.35913, 0.39246,&
0.42650, 0.46119, 0.49538, 0.52941, 0.56250,&
0.59510, 0.63037, 0.66574, 0.69774, 0.72973,&
0.75999, 0.77280, 0.75992, 0.76224, 0.76317,&
0.76352, 0.76357, 0.76358, 0.76349 /)
!
!* pressure of the segments ends (1st point is takeoff, last point is landing)
! (pascals)
!
WAUTELET Philippe
committed
IF (TAIRCRAFTS(2)%ALTDEF) THEN
ALLOCATE(TAIRCRAFTS(2)%SEGP (TAIRCRAFTS(2)%SEG+1))
TAIRCRAFTS(2)%SEGP = 100. * (/1001.,1001.0, 989.2, 987.5, 987.5,&
524
525
526
527
528
529
530
531
532
533
534
535
536
537
538
539
540
541
542
543
544
545
546
547
548
549
550
551
552
553
554
555
556
557
558
559
560
561
562
563
987.9, 989.1, 990.2, 989.3, 988.6,&
989.8, 989.6, 991.0, 986.1, 980.7,&
986.5, 991.9, 991.5, 993.0, 992.1,&
991.3, 991.8, 982.3, 972.0, 960.0,&
950.5, 938.4, 924.8, 911.7, 899.5,&
886.9, 876.2, 864.0, 849.9, 843.7,&
852.1, 861.8, 871.3, 880.8, 891.3,&
901.5, 913.5, 926.8, 940.6, 952.3,&
952.9, 938.6, 921.6, 907.2, 898.2,&
884.6, 880.2, 892.0, 902.0, 916.1,&
931.1, 926.4, 909.7, 897.0, 891.0,&
880.8, 868.3, 861.0, 851.4, 842.2,&
833.7, 823.2, 809.5, 799.0, 789.0,&
778.7, 768.7, 759.3, 761.1, 774.5,&
789.5, 809.8, 829.7, 841.2, 856.2,&
871.5, 886.9, 904.8, 923.0, 937.5,&
952.0, 965.7, 980.8, 985.2, 988.0,&
987.3, 985.8, 986.6, 989.8, 990.7,&
991.4, 990.5, 989.1, 988.2, 988.0,&
984.7, 985.0, 977.8, 964.8, 952.8,&
941.3, 929.7, 918.2, 909.4, 915.3,&
928.5, 943.0, 961.3, 978.0, 989.2,&
992.9, 994.5, 994.4, 987.9, 974.2,&
960.6, 946.6, 933.5, 920.8, 908.2,&
895.7, 883.6, 872.7, 861.4, 850.0,&
837.7, 825.8, 814.0, 803.1, 796.9,&
803.0, 812.6, 824.4, 841.8, 859.3,&
876.9, 893.8, 910.1, 928.2, 942.5,&
962.5, 978.7, 964.3, 951.7, 937.5,&
921.1, 906.0, 891.0, 879.2, 862.9,&
847.7, 836.1, 826.2, 814.5, 802.0,&
806.3, 820.0, 836.0, 853.4, 870.7,&
889.7, 909.7, 929.1, 950.2, 971.8,&
988.8, 993.3, 992.3, 991.9, 991.4,&
992.0, 991.7, 988.2, 986.2, 989.9,&
990.5, 991.2, 989.3, 988.5, 988.2,&
986.8, 986.4, 987.0, 981.0, 975.5,&
975.8, 993.9,1004.1,1004.1,1004.1,&
1004.1,1004.1,1004.1,1004.1 /)
ELSE
WAUTELET Philippe
committed
ALLOCATE(TAIRCRAFTS(2)%SEGZ (TAIRCRAFTS(2)%SEG+1))
TAIRCRAFTS(2)%SEGZ = (/8000,8000,8000,8000,8000,&
566
567
568
569
570
571
572
573
574
575
576
577
578
579
580
581
582
583
584
585
586
587
588
589
590
591
592
593
594
595
596
597
598
599
600
601
602
603
604
605
606
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000 /)
ENDIF
!
WAUTELET Philippe
committed
IF ( NAIRCRAFTS < 3 ) RETURN
#else
CALL PRINT_MSG( NVERB_FATAL, 'GEN', 'INI_AIRCRAFT', 'aircraft characteristics are commented' )
#endif
!----------------------------------------------------------------------------
!
!* 1. Aircraft number 3
! -----------------
WAUTELET Philippe
committed
#if 0
WAUTELET Philippe
committed
TAIRCRAFTS(3)%NMODEL = 0
WAUTELET Philippe
committed
TAIRCRAFTS(3)%MODEL = 'FIX'
WAUTELET Philippe
committed
TAIRCRAFTS(3)%TYPE = 'AIRCRA'
WAUTELET Philippe
committed
TAIRCRAFTS(3)%TITLE = 'SAAL19A'
!
!* time step for storage
!
WAUTELET Philippe
committed
TAIRCRAFTS(3)%TFLYER_TIME%XTSTEP = 30.
!
!* take-off date and time
!
WAUTELET Philippe
committed
TAIRCRAFTS(3)%LAUNCH%nyear = 2007
TAIRCRAFTS(3)%LAUNCH%nmonth = 04
TAIRCRAFTS(3)%LAUNCH%nday = 19
TAIRCRAFTS(3)%LAUNCH%xtime = 45369
!
!* number of flight segments
!
WAUTELET Philippe
committed
TAIRCRAFTS(3)%SEG = 39
!
!* initalisation of flag for pressure (T) or Z(F) for aicraft altitude
!
WAUTELET Philippe
committed
TAIRCRAFTS(3)%ALTDEF = .TRUE.
!
!* allocation of the arrays
!
WAUTELET Philippe
committed
ALLOCATE(TAIRCRAFTS(3)%SEGTIME(TAIRCRAFTS(3)%SEG ))
ALLOCATE(TAIRCRAFTS(3)%SEGLAT (TAIRCRAFTS(3)%SEG+1))
ALLOCATE(TAIRCRAFTS(3)%SEGLON (TAIRCRAFTS(3)%SEG+1))
!
!* duration of the segments (seconds)
!
WAUTELET Philippe
committed
TAIRCRAFTS(3)%SEGTIME = (/ 15, 16, 16, 18, 17, 17,&
22, 25, 19, 19, 22, 27,&
28, 27, 29, 32, 30, 24,&
169, 18, 15, 18, 17, 16,&
16, 14, 14, 18, 17, 15,&
14, 14, 19, 20, 16, 15,&
14, 16, 21 /)
!
!* latitudes of the segments ends (1st point is takeoff, last point is landing)
! (decimal degrees)
!
WAUTELET Philippe
committed
TAIRCRAFTS(3)%SEGLAT = (/ 44.14451, 44.14084, 44.14068, 44.14479, 44.14884,&
44.14843, 44.14437, 44.14127, 44.14574, 44.14858,&
44.14655, 44.14130, 44.14384, 44.14738, 44.14158,&
44.14245, 44.14607, 44.14023, 44.14227, 44.15136,&
44.14792, 44.14352, 44.13874, 44.13904, 44.14350,&
44.14701, 44.14614, 44.14223, 44.14001, 44.14320,&
44.14671, 44.14661, 44.14324, 44.14091, 44.14492,&
44.14721, 44.14510, 44.14152, 44.14219, 44.14698 /)
!
!* longitudes of the segments ends (1st point is takeoff, last point is landing)
! (decimal degrees)
!
WAUTELET Philippe
committed
TAIRCRAFTS(3)%SEGLON = (/0.95322, 0.95562, 0.96155, 0.96490, 0.96186,&
0.95576, 0.95421, 0.96105, 0.96593, 0.96076,&
0.95485, 0.95618, 0.96341, 0.95769, 0.95681,&
0.96585, 0.96073, 0.96158, 0.97041, 0.96299,&
0.95662, 0.95481, 0.95871, 0.96586, 0.96804,&
0.96407, 0.95952, 0.95957, 0.96608, 0.97088,&
0.96825, 0.96292, 0.96078, 0.96622, 0.96953,&
0.96476, 0.96053, 0.96218, 0.96765, 0.96600 /)
!
!* pressure of the segments ends (1st point is takeoff, last point is landing)
! (pascals)
!
WAUTELET Philippe
committed
IF (TAIRCRAFTS(3)%ALTDEF) THEN
ALLOCATE(TAIRCRAFTS(3)%SEGP (TAIRCRAFTS(3)%SEG+1))
TAIRCRAFTS(3)%SEGP = 100. * (/ 992.5, 987.4, 982.1, 976.4, 969.3,&
964.3, 958.4, 952.9, 947.5, 942.8,&
936.5, 930.8, 925.6, 919.8, 914.6,&
909.2, 903.6, 898.0, 893.0, 881.8,&
887.3, 892.5, 897.8, 903.1, 908.6,&
914.1, 919.2, 924.9, 929.5, 935.2,&
940.4, 946.6, 951.8, 957.8, 963.1,&
969.1, 974.1, 980.0, 986.0, 993.0 /)
ELSE
WAUTELET Philippe
committed
ALLOCATE(TAIRCRAFTS(3)%SEGZ (TAIRCRAFTS(3)%SEG+1))
TAIRCRAFTS(3)%SEGZ = (/8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000 /)
ENDIF
!
WAUTELET Philippe
committed
IF ( NAIRCRAFTS < 4 ) RETURN
#else
CALL PRINT_MSG( NVERB_FATAL, 'GEN', 'INI_AIRCRAFT', 'aircraft characteristics are commented' )
#endif
!----------------------------------------------------------------------------
!
!* 1. Aircraft number 4
! -----------------
WAUTELET Philippe
committed
#if 0
WAUTELET Philippe
committed
TAIRCRAFTS(4)%NMODEL = 0
WAUTELET Philippe
committed
TAIRCRAFTS(4)%MODEL = 'FIX'
WAUTELET Philippe
committed
TAIRCRAFTS(4)%TYPE = 'AIRCRA'
WAUTELET Philippe
committed
TAIRCRAFTS(4)%TITLE = 'SAAL19B'
!
!* time step for storage
!
WAUTELET Philippe
committed
TAIRCRAFTS(4)%TFLYER_TIME%XTSTEP = 30.
!
!* take-off date and time
!
WAUTELET Philippe
committed
TAIRCRAFTS(4)%LAUNCH%nyear = 2007
TAIRCRAFTS(4)%LAUNCH%nmonth = 04
TAIRCRAFTS(4)%LAUNCH%nday = 19
TAIRCRAFTS(4)%LAUNCH%xtime = 60392.
!
!* number of flight segments
!
WAUTELET Philippe
committed
TAIRCRAFTS(4)%SEG = 39
!
!* initalisation of flag for pressure (T) or Z(F) for aicraft altitude
!
WAUTELET Philippe
committed
TAIRCRAFTS(4)%ALTDEF = .TRUE.
!
!* allocation of the arrays
!
WAUTELET Philippe
committed
ALLOCATE(TAIRCRAFTS(4)%SEGTIME(TAIRCRAFTS(4)%SEG ))
ALLOCATE(TAIRCRAFTS(4)%SEGLAT (TAIRCRAFTS(4)%SEG+1))
ALLOCATE(TAIRCRAFTS(4)%SEGLON (TAIRCRAFTS(4)%SEG+1))
!
!* duration of the segments (seconds)
!
WAUTELET Philippe
committed
TAIRCRAFTS(4)%SEGTIME = (/ 36, 18, 18, 21, 24, 23,&
20, 20, 25, 27, 21, 25,&
27, 23, 21, 23, 25, 21,&
27, 190, 17, 17, 18, 17,&
18, 17, 15, 18, 22, 17,&
16, 18, 22, 22, 19, 20,&
21, 23, 22 /)
!
!* latitudes of the segments ends (1st point is takeoff, last point is landing)
! (decimal degrees)
!
WAUTELET Philippe
committed
TAIRCRAFTS(4)%SEGLAT = (/ 44.14025, 44.13824, 44.14291, 44.14575, 44.14321,&
44.13749, 44.13853, 44.14373, 44.14530, 44.13921,&
44.13773, 44.14285, 44.13974, 44.13622, 44.14093,&
44.14375, 44.13868, 44.13771, 44.14272, 44.14156,&
44.14130, 44.14335, 44.14031, 44.13480, 44.13150,&
44.13157, 44.13507, 44.13921, 44.14201, 44.13823,&
44.13479, 44.13668, 44.14132, 44.14112, 44.13621,&
44.13775, 44.14254, 44.14194, 44.13669, 44.13837 /)
!
!* longitudes of the segments ends (1st point is takeoff, last point is landing)
! (decimal degrees)
!
WAUTELET Philippe
committed
TAIRCRAFTS(4)%SEGLON = (/ 0.94868, 0.95712, 0.95820, 0.95265, 0.94556,&
0.94730, 0.95518, 0.95559, 0.94882, 0.94656,&
0.95488, 0.95463, 0.94889, 0.95589, 0.95988,&
0.95389, 0.95076, 0.95834, 0.95888, 0.95095,&
0.95897, 0.95259, 0.94684, 0.94743, 0.95294,&
0.96042, 0.96527, 0.96527, 0.95949, 0.95413,&
0.95842, 0.96350, 0.96231, 0.95483, 0.95597,&
0.96187, 0.96037, 0.95264, 0.95278, 0.95857 /)
!
!* pressure of the segments ends (1st point is takeoff, last point is landing)
! (pascals)
!
WAUTELET Philippe
committed
IF (TAIRCRAFTS(4)%ALTDEF) THEN
ALLOCATE(TAIRCRAFTS(4)%SEGP (TAIRCRAFTS(4)%SEG+1))
TAIRCRAFTS(4)%SEGP = 100. * (/ 992.3, 985.4, 979.9, 974.2, 969.2,&
962.8, 957.7, 952.1, 946.3, 940.5,&
935.3, 930.4, 924.0, 918.9, 913.4,&
907.8, 902.8, 897.1, 892.2, 886.3,&
881.6, 886.6, 891.9, 897.0, 902.3,&
907.9, 912.8, 918.3, 924.0, 929.0,&
934.6, 940.3, 946.0, 951.4, 956.5,&
962.8, 968.1, 973.7, 979.3, 984.9 /)
ELSE
WAUTELET Philippe
committed
ALLOCATE(TAIRCRAFTS(4)%SEGZ (TAIRCRAFTS(4)%SEG+1))
TAIRCRAFTS(4)%SEGZ = (/8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000/)
ENDIF
!
WAUTELET Philippe
committed
IF ( NAIRCRAFTS < 5 ) RETURN
#else
CALL PRINT_MSG( NVERB_FATAL, 'GEN', 'INI_AIRCRAFT', 'aircraft characteristics are commented' )
#endif
!----------------------------------------------------------------------------
!
!* 1. Aircraft number 5
! -----------------
WAUTELET Philippe
committed
#if 0
WAUTELET Philippe
committed
TAIRCRAFTS(5)%NMODEL = 0
WAUTELET Philippe
committed
TAIRCRAFTS(5)%MODEL = 'FIX'
WAUTELET Philippe
committed
TAIRCRAFTS(5)%TYPE = 'AIRCRA'
WAUTELET Philippe
committed
TAIRCRAFTS(5)%TITLE = 'SAIB19A'
!
!* time step for storage
!
WAUTELET Philippe
committed
TAIRCRAFTS(5)%TFLYER_TIME%XTSTEP = 30.
!
!* take-off date and time
!
WAUTELET Philippe
committed
TAIRCRAFTS(5)%LAUNCH%nyear = 2007
TAIRCRAFTS(5)%LAUNCH%nmonth = 04
TAIRCRAFTS(5)%LAUNCH%nday = 19
TAIRCRAFTS(5)%LAUNCH%xtime = 43380.
!
!* number of flight segments
!
WAUTELET Philippe
committed
TAIRCRAFTS(5)%SEG = 176
!
!* initalisation of flag for pressure (T) or Z(F) for aicraft altitude
!
WAUTELET Philippe
committed
TAIRCRAFTS(5)%ALTDEF = .TRUE.
!
!* allocation of the arrays
!
WAUTELET Philippe
committed
ALLOCATE(TAIRCRAFTS(5)%SEGTIME(TAIRCRAFTS(5)%SEG ))
ALLOCATE(TAIRCRAFTS(5)%SEGLAT (TAIRCRAFTS(5)%SEG+1))
ALLOCATE(TAIRCRAFTS(5)%SEGLON (TAIRCRAFTS(5)%SEG+1))
!
!* duration of the segments (seconds)
!
WAUTELET Philippe
committed
TAIRCRAFTS(5)%SEGTIME = (/ 28, 28, 29, 29, 29, 28,&
882
883
884
885
886
887
888
889
890
891
892
893
894
895
896
897
898
899
900
901
902
903
904
905
906
907
908
909
910
911
912
913
914
915
28, 28, 29, 26, 28, 27,&
28, 27, 28, 27, 25, 27,&
27, 26, 24, 25, 26, 26,&
24, 25, 27, 27, 25, 27,&
27, 28, 27, 28, 27, 27,&
28, 28, 27, 28, 28, 28,&
28, 28, 28, 27, 28, 26,&
27, 27, 27, 26, 25, 25,&
27, 27, 26, 25, 28, 28,&
28, 27, 29, 27, 27, 28,&
29, 27, 27, 27, 27, 26,&
26, 26, 26, 25, 26, 26,&
26, 27, 26, 25, 26, 25,&
26, 25, 25, 25, 26, 25,&
24, 25, 25, 25, 25, 24,&
26, 26, 25, 25, 25, 26,&
24, 23, 23, 24, 25, 22,&
21, 24, 25, 24, 24, 24,&
24, 24, 26, 26, 24, 26,&
26, 25, 25, 27, 25, 25,&
25, 25, 24, 24, 25, 24,&
25, 24, 24, 24, 24, 25,&
24, 24, 23, 25, 25, 24,&
23, 25, 27, 26, 24, 25,&
27, 27, 26, 26, 26, 25,&
25, 26, 25, 25, 25, 25,&
25, 26, 26, 25, 25, 25,&
26, 26, 25, 25, 25, 25,&
25, 25 /)
!
!* latitudes of the segments ends (1st point is takeoff, last point is landing)
! (decimal degrees)
!
WAUTELET Philippe
committed
TAIRCRAFTS(5)%SEGLAT = (/44.38992, 44.38830, 44.38713, 44.38609, 44.38512,&
917
918
919
920
921
922
923
924
925
926
927
928
929
930
931
932
933
934
935
936
937
938
939
940
941
942
943
944
945
946
947
948
949
950
951
952
953
954
955
956
44.38420, 44.38336, 44.38248, 44.38151, 44.38046,&
44.37942, 44.37835, 44.37729, 44.37630, 44.37530,&
44.37407, 44.37156, 44.36766, 44.36184, 44.35421,&
44.34673, 44.33986, 44.33271, 44.32536, 44.31800,&
44.31084, 44.30350, 44.29764, 44.29618, 44.29837,&
44.30431, 44.31233, 44.32061, 44.32872, 44.33691,&
44.34478, 44.35284, 44.36091, 44.36894, 44.37666,&
44.38478, 44.39273, 44.40079, 44.40907, 44.41711,&
44.42513, 44.43278, 44.44096, 44.44872, 44.45604,&
44.46205, 44.46722, 44.47121, 44.47528, 44.47961,&
44.48401, 44.48833, 44.49243, 44.49633, 44.50052,&
44.50473, 44.50888, 44.51291, 44.51712, 44.52108,&
44.52521, 44.52945, 44.53390, 44.53808, 44.54208,&
44.54610, 44.55014, 44.55407, 44.55854, 44.56353,&
44.56913, 44.57520, 44.58130, 44.58722, 44.59335,&
44.59960, 44.60600, 44.61232, 44.61881, 44.62519,&
44.63163, 44.63794, 44.64420, 44.65037, 44.65659,&
44.66282, 44.66911, 44.67549, 44.68206, 44.68845,&
44.69469, 44.70078, 44.70619, 44.70841, 44.70754,&
44.70336, 44.69652, 44.68935, 44.68254, 44.67577,&
44.66869, 44.66101, 44.65345, 44.64679, 44.64044,&
44.63337, 44.62587, 44.61864, 44.61169, 44.60483,&
44.59803, 44.59103, 44.58360, 44.57622, 44.56934,&
44.56229, 44.55523, 44.54845, 44.54173, 44.53448,&
44.52751, 44.52062, 44.51361, 44.50655, 44.49974,&
44.49290, 44.48547, 44.47823, 44.47103, 44.46391,&
44.45718, 44.45013, 44.44316, 44.43579, 44.42883,&
44.42169, 44.41486, 44.40771, 44.40028, 44.39341,&
44.38669, 44.37949, 44.37202, 44.36499, 44.35838,&
44.35147, 44.34417, 44.33688, 44.32985, 44.32279,&
44.31593, 44.30918, 44.30215, 44.29464, 44.28732,&
44.27999, 44.27291, 44.26616, 44.25944, 44.25235,&
44.24517, 44.23800, 44.23081, 44.22393, 44.21662,&
44.20946, 44.20266, 44.19582, 44.18895, 44.18196,&
44.17498, 44.16789 /)
!
!* longitudes of the segments ends (1st point is takeoff, last point is landing)
! (decimal degrees)
!
WAUTELET Philippe
committed
TAIRCRAFTS(5)%SEGLON = (/ 0.60996, 0.59790, 0.58554, 0.57296, 0.56046,&
958
959
960
961
962
963
964
965
966
967
968
969
970
971
972
973
974
975
976
977
978
979
980
981
982
983
984
985
986
987
988
989
990
991
992
993
994
995
996
997
0.54813, 0.53613, 0.52410, 0.51125, 0.49815,&
0.48593, 0.47312, 0.46084, 0.44829, 0.43635,&
0.42374, 0.41321, 0.40397, 0.39536, 0.38761,&
0.37986, 0.37280, 0.36554, 0.35794, 0.35061,&
0.34350, 0.33612, 0.32785, 0.32066, 0.31451,&
0.30861, 0.30376, 0.29840, 0.29296, 0.28726,&
0.28162, 0.27583, 0.26994, 0.26423, 0.25891,&
0.25323, 0.24778, 0.24212, 0.23624, 0.23064,&
0.22502, 0.21967, 0.21392, 0.20841, 0.20143,&
0.19328, 0.18381, 0.17339, 0.16261, 0.15162,&
0.14002, 0.12849, 0.11740, 0.10678, 0.09554,&
0.08426, 0.07307, 0.06239, 0.05099, 0.04032,&
0.02923, 0.01810, 0.00646,-0.00451,-0.01539,&
-0.02655,-0.03777,-0.04874,-0.05951,-0.06992,&
-0.08001,-0.08912,-0.09831,-0.10747,-0.11645,&
-0.12552,-0.13428,-0.14260,-0.15142,-0.16039,&
-0.16949,-0.17857,-0.18770,-0.19650,-0.20544,&
-0.21419,-0.22292,-0.23212,-0.24134,-0.25051,&
-0.25963,-0.26837,-0.27772,-0.28662,-0.29513,&
-0.30338,-0.31122,-0.31934,-0.32710,-0.33460,&
-0.34242,-0.35080,-0.35914,-0.36639,-0.37351,&
-0.38158,-0.38999,-0.39802,-0.40577,-0.41337,&
-0.42071,-0.42825,-0.43635,-0.44428,-0.45168,&
-0.45980,-0.46756,-0.47507,-0.48266,-0.49060,&
-0.49836,-0.50612,-0.51447,-0.52244,-0.53007,&
-0.53764,-0.54520,-0.55282,-0.56051,-0.56820,&
-0.57580,-0.58375,-0.59147,-0.59952,-0.60706,&
-0.61472,-0.62227,-0.63041,-0.63860,-0.64631,&
-0.65352,-0.66121,-0.66938,-0.67724,-0.68459,&
-0.69224,-0.70005,-0.70780,-0.71548,-0.72306,&
-0.73052,-0.73777,-0.74522,-0.75335,-0.76142,&
-0.76949,-0.77717,-0.78452,-0.79186,-0.79943,&
-0.80743,-0.81530,-0.82307,-0.83074,-0.83852,&
-0.84620,-0.85372,-0.86115,-0.86912,-0.87743,&
-0.88529,-0.89333 /)
!
!
!* pressure of the segments ends (1st point is takeoff, last point is landing)
! (pascals)
!
WAUTELET Philippe
committed
IF (TAIRCRAFTS(5)%ALTDEF) THEN
ALLOCATE(TAIRCRAFTS(5)%SEGP (TAIRCRAFTS(5)%SEG+1))
TAIRCRAFTS(5)%SEGP = 100. * (/ 995.7, 998.1, 998.7, 998.8, 999.1,&