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source: palm/trunk/SOURCE/virtual_flight_mod.f90 @ 4830

Last change on this file since 4830 was 4828, checked in by Giersch, 4 years ago
Copyright updated to year 2021, interface pmc_sort removed to accelarate the nesting code
Property svn:keywords set to `Id`
File size: 47.2 KB

Rev	Line
[1957]	1	!> @file virtual_flights_mod.f90
[4497]	2	!--------------------------------------------------------------------------------------------------!
[2696]	3	! This file is part of the PALM model system.
[1957]	4	!
[4497]	5	! PALM is free software: you can redistribute it and/or modify it under the terms of the GNU General
	6	! Public License as published by the Free Software Foundation, either version 3 of the License, or
	7	! (at your option) any later version.
[1957]	8	!
[4497]	9	! PALM is distributed in the hope that it will be useful, but WITHOUT ANY WARRANTY; without even the
	10	! implied warranty of MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU General
	11	! Public License for more details.
[1957]	12	!
[4497]	13	! You should have received a copy of the GNU General Public License along with PALM. If not, see
	14	! <http://www.gnu.org/licenses/>.
[1957]	15	!
[4828]	16	! Copyright 1997-2021 Leibniz Universitaet Hannover
[4497]	17	!--------------------------------------------------------------------------------------------------!
[1957]	18	!
[4497]	19	!
[1957]	20	! Current revisions:
[4497]	21	! -----------------
[1957]	22	!
[3049]	23	!
[1957]	24	! Former revisions:
	25	! -----------------
	26	! $Id: virtual_flight_mod.f90 4828 2021-01-05 11:21:41Z Giersch $
[4541]	27	! Bugfix, use time_since_reference_point instead of simulated_time
	28	!
	29	! 4535 2020-05-15 12:07:23Z raasch
[4535]	30	! bugfix for restart data format query
	31	!
	32	! 4522 2020-05-06 14:17:05Z suehring
[4522]	33	! Modularize user_init_flight in order to provide an explicit interface.
	34	!
	35	! 4497 2020-04-15 10:20:51Z raasch
[4497]	36	! file re-formatted to follow the PALM coding standard
	37	!
	38	!
	39	! 4495 2020-04-13 20:11:20Z raasch
[4495]	40	! restart data handling with MPI-IO added
	41	!
	42	! 4360 2020-01-07 11:25:50Z suehring
[4182]	43	! Corrected "Former revisions" section
[4497]	44	!
[4182]	45	! 4004 2019-05-24 11:32:38Z suehring
[4004]	46	! Allow variable start- and end locations also in return mode
[4497]	47	!
[4004]	48	! 3885 2019-04-11 11:29:34Z kanani
[4497]	49	! Changes related to global restructuring of location messages and introduction of additional
	50	! debug messages
	51	!
[3885]	52	! 3655 2019-01-07 16:51:22Z knoop
[3547]	53	! variables documented
[4497]	54	!
[4182]	55	! 1957 2016-07-07 10:43:48Z suehring
	56	! Initial revision
[2716]	57	!
[1957]	58	! Description:
	59	! ------------
	60	!> Module for virtual flight measurements.
[2271]	61	!> @todo Err msg PA0438: flight can be inside topography -> extra check?
[4497]	62	!--------------------------------------------------------------------------------------------------!
[1957]	63	MODULE flight_mod
[4497]	64
[4495]	65	USE control_parameters, &
[4497]	66	ONLY: debug_output, &
	67	fl_max, num_leg, &
	68	num_var_fl, &
	69	num_var_fl_user, &
	70	restart_data_format_output, &
	71	virtual_flight
	72
[1957]	73	USE kinds
	74
[4495]	75	USE restart_data_mpi_io_mod, &
	76	ONLY: rd_mpi_io_check_array, rrd_mpi_io_global_array, wrd_mpi_io_global_array
	77
[4522]	78	USE user_init_flight_mod, &
	79	ONLY: user_init_flight
[4495]	80
[4522]	81
[4497]	82	CHARACTER(LEN=6), DIMENSION(fl_max) :: leg_mode = 'cyclic' !< flight mode through the model domain, either 'cyclic' or
	83	!<'return'
[1957]	84
	85	INTEGER(iwp) :: l !< index for flight leg
	86	INTEGER(iwp) :: var_index !< index for measured variable
	87
[4497]	88	LOGICAL, DIMENSION(:), ALLOCATABLE :: cyclic_leg !< flag to identify fly mode
[1957]	89
	90	REAL(wp) :: flight_end = 9999999.9_wp !< end time of virtual flight
	91	REAL(wp) :: flight_begin = 0.0_wp !< end time of virtual flight
	92
[4497]	93	REAL(wp), DIMENSION(fl_max) :: flight_angle = 45.0_wp !< angle determining the horizontal flight direction
	94	REAL(wp), DIMENSION(fl_max) :: flight_level = 100.0_wp !< flight level
	95	REAL(wp), DIMENSION(fl_max) :: max_elev_change = 0.0_wp !< maximum elevation change for the respective flight leg
	96	REAL(wp), DIMENSION(fl_max) :: rate_of_climb = 0.0_wp !< rate of climb or descent
	97	REAL(wp), DIMENSION(fl_max) :: speed_agl = 25.0_wp !< absolute horizontal flight speed above ground level (agl)
	98	REAL(wp), DIMENSION(fl_max) :: x_start = 999999999.0_wp !< start x position
	99	REAL(wp), DIMENSION(fl_max) :: x_end = 999999999.0_wp !< end x position
	100	REAL(wp), DIMENSION(fl_max) :: y_start = 999999999.0_wp !< start y position
	101	REAL(wp), DIMENSION(fl_max) :: y_end = 999999999.0_wp !< end y position
[1957]	102
[4497]	103	REAL(wp), DIMENSION(:), ALLOCATABLE :: u_agl !< u-component of flight speed
	104	REAL(wp), DIMENSION(:), ALLOCATABLE :: v_agl !< v-component of flight speed
	105	REAL(wp), DIMENSION(:), ALLOCATABLE :: w_agl !< w-component of flight speed
	106	REAL(wp), DIMENSION(:), ALLOCATABLE :: x_pos !< aircraft x-position
	107	REAL(wp), DIMENSION(:), ALLOCATABLE :: y_pos !< aircraft y-position
	108	REAL(wp), DIMENSION(:), ALLOCATABLE :: z_pos !< aircraft z-position
[1957]	109
[4497]	110	REAL(wp), DIMENSION(:,:), ALLOCATABLE :: sensor_l !< measured data on local PE
	111	REAL(wp), DIMENSION(:,:), ALLOCATABLE :: sensor !< measured data
[1957]	112
	113	REAL(wp), DIMENSION(:,:,:), ALLOCATABLE :: var_u !< dummy array for possibly user-defined quantities
	114
	115	SAVE
	116
	117	PRIVATE
	118
	119	INTERFACE flight_header
	120	MODULE PROCEDURE flight_header
	121	END INTERFACE flight_header
[4497]	122
[1957]	123	INTERFACE flight_init
	124	MODULE PROCEDURE flight_init
	125	END INTERFACE flight_init
	126
	127	INTERFACE flight_init_output
	128	MODULE PROCEDURE flight_init_output
	129	END INTERFACE flight_init_output
	130
	131	INTERFACE flight_check_parameters
	132	MODULE PROCEDURE flight_check_parameters
	133	END INTERFACE flight_check_parameters
	134
	135	INTERFACE flight_parin
	136	MODULE PROCEDURE flight_parin
	137	END INTERFACE flight_parin
	138
	139	INTERFACE interpolate_xyz
	140	MODULE PROCEDURE interpolate_xyz
	141	END INTERFACE interpolate_xyz
	142
	143	INTERFACE flight_measurement
	144	MODULE PROCEDURE flight_measurement
	145	END INTERFACE flight_measurement
[4497]	146
	147	INTERFACE flight_rrd_global
[4495]	148	MODULE PROCEDURE flight_rrd_global_ftn
	149	MODULE PROCEDURE flight_rrd_global_mpi
[2894]	150	END INTERFACE flight_rrd_global
[1957]	151
[4497]	152	INTERFACE flight_wrd_global
	153	MODULE PROCEDURE flight_wrd_global
	154	END INTERFACE flight_wrd_global
	155
[1957]	156	!
	157	!-- Private interfaces
[4497]	158	PRIVATE flight_check_parameters, &
	159	flight_init_output, &
	160	interpolate_xyz
[1957]	161	!
	162	!-- Public interfaces
[4497]	163	PUBLIC flight_init, &
	164	flight_header, &
	165	flight_parin, &
	166	flight_measurement, &
	167	flight_wrd_global, &
	168	flight_rrd_global
[1957]	169	!
	170	!-- Public variables
[4497]	171	PUBLIC fl_max, &
	172	sensor, &
	173	x_pos, &
	174	y_pos, &
	175	z_pos
[1957]	176
	177	CONTAINS
	178
[4497]	179	!--------------------------------------------------------------------------------------------------!
[1957]	180	! Description:
	181	! ------------
	182	!> Header output for flight module.
[4497]	183	!--------------------------------------------------------------------------------------------------!
	184	SUBROUTINE flight_header ( io )
[1957]	185
	186
[4497]	187	IMPLICIT NONE
[1957]	188
[4497]	189	INTEGER(iwp), INTENT(IN) :: io !< Unit of the output file
[1957]	190
[4497]	191	WRITE ( io, 1 )
	192	WRITE ( io, 2 )
	193	WRITE ( io, 3 ) num_leg
	194	WRITE ( io, 4 ) flight_begin
	195	WRITE ( io, 5 ) flight_end
	196
	197	DO l=1, num_leg
	198	WRITE ( io, 6 ) l
	199	WRITE ( io, 7 ) speed_agl(l)
	200	WRITE ( io, 8 ) flight_level(l)
	201	WRITE ( io, 9 ) max_elev_change(l)
	202	WRITE ( io, 10 ) rate_of_climb(l)
	203	WRITE ( io, 11 ) leg_mode(l)
	204	ENDDO
	205
	206
	207	1 FORMAT (' Virtual flights: ----------------' )
	208	2 FORMAT (' Output every timestep' )
	209	3 FORMAT (' Number of flight legs:', I3 )
	210	4 FORMAT (' Begin of measurements:', F10.1 , ' s' )
	211	5 FORMAT (' End of measurements:', F10.1 , ' s' )
	212	6 FORMAT (' Leg', I3/, ' ------' )
	213	7 FORMAT (' Flight speed : ', F5.1, ' m/s' )
	214	8 FORMAT (' Flight level : ', F5.1, ' m' )
	215	9 FORMAT (' Maximum elevation change: ', F5.1, ' m/s' )
	216	10 FORMAT (' Rate of climb / descent : ', F5.1, ' m/s' )
	217	11 FORMAT (' Leg mode : ', A/ )
	218
	219	END SUBROUTINE flight_header
	220
	221	!--------------------------------------------------------------------------------------------------!
[1957]	222	! Description:
	223	! ------------
	224	!> Reads the namelist flight_par.
[4497]	225	!--------------------------------------------------------------------------------------------------!
	226	SUBROUTINE flight_parin
[1957]	227
[4497]	228	USE control_parameters, &
	229	ONLY: message_string
[1957]	230
[4497]	231	IMPLICIT NONE
[1957]	232
[4497]	233	CHARACTER(LEN=80) :: line !< dummy string that contains the current line of the parameter file
[2932]	234
[4497]	235	NAMELIST /flight_par/ flight_angle, &
	236	flight_begin, &
	237	flight_end, &
	238	flight_level, &
	239	leg_mode, &
	240	max_elev_change, &
	241	rate_of_climb, &
	242	speed_agl, &
	243	x_end, &
	244	x_start, &
	245	y_end, &
	246	y_start
	247
	248
	249	NAMELIST /virtual_flight_parameters/ flight_angle, &
	250	flight_begin, &
	251	flight_end, &
	252	flight_level, &
	253	leg_mode, &
	254	max_elev_change, &
	255	rate_of_climb, &
	256	speed_agl, &
	257	x_end, &
	258	x_start, &
	259	y_end, &
	260	y_start
[1957]	261	!
[4497]	262	!-- Try to find the namelist flight_par
	263	REWIND ( 11 )
	264	line = ' '
	265	DO WHILE ( INDEX( line, '&virtual_flight_parameters' ) == 0 )
	266	READ ( 11, '(A)', END = 12 ) line
	267	ENDDO
	268	BACKSPACE ( 11 )
[1957]	269
	270	!
[4497]	271	!-- Read namelist
	272	READ ( 11, virtual_flight_parameters, ERR = 10 )
[2932]	273	!
[4497]	274	!-- Set switch so that virtual flights shall be carried out
	275	virtual_flight = .TRUE.
[2932]	276
[4497]	277	GOTO 14
[3246]	278
	279	10 BACKSPACE( 11 )
[3248]	280	READ( 11 , '(A)') line
	281	CALL parin_fail_message( 'virtual_flight_parameters', line )
[2932]	282	!
	283	!-- Try to find the old namelist
[3246]	284	12 REWIND ( 11 )
[2932]	285	line = ' '
[4497]	286	DO WHILE ( INDEX( line, '&flight_par' ) == 0 )
	287	READ ( 11, '(A)', END = 14 ) line
[2932]	288	ENDDO
	289	BACKSPACE ( 11 )
	290
	291	!
[4497]	292	!-- Read namelist
	293	READ ( 11, flight_par, ERR = 13, END = 14 )
	294
	295	message_string = 'namelist flight_par is deprecated and will be ' // &
	296	'removed in near future.& Please use namelist ' // &
	297	'virtual_flight_parameters instead'
	298	CALL message( 'flight_parin', 'PA0487', 0, 1, 0, 6, 0 )
[1957]	299	!
[4497]	300	!-- Set switch so that virtual flights shall be carried out
	301	virtual_flight = .TRUE.
[1957]	302
[4497]	303	GOTO 14
[2563]	304
[3246]	305	13 BACKSPACE( 11 )
[3248]	306	READ( 11 , '(A)') line
	307	CALL parin_fail_message( 'flight_par', line )
[3246]	308
	309	14 CONTINUE
	310
[4497]	311	END SUBROUTINE flight_parin
[1957]	312
[4497]	313	!--------------------------------------------------------------------------------------------------!
[1957]	314	! Description:
	315	! ------------
[4497]	316	!> Inititalization of required arrays, number of legs and flags. Moreover, initialize flight speed
	317	!> and -direction, as well as start positions.
	318	!--------------------------------------------------------------------------------------------------!
	319	SUBROUTINE flight_init
[1957]	320
[4497]	321	USE basic_constants_and_equations_mod, &
	322	ONLY: pi
[1957]	323
[4497]	324	USE control_parameters, &
	325	ONLY: initializing_actions
[3885]	326
[4497]	327	USE indices, &
	328	ONLY: nxlg, &
	329	nxrg, &
	330	nysg, &
	331	nyng, &
	332	nzb, &
	333	nzt
[3885]	334
[4497]	335	IMPLICIT NONE
	336
	337	REAL(wp) :: distance !< distance between start and end position of a flight leg
	338
	339
	340	IF ( debug_output ) CALL debug_message( 'flight_init', 'start' )
[1957]	341	!
[4497]	342	!-- Determine the number of flight legs
	343	l = 1
	344	DO WHILE ( x_start(l) /= 999999999.0_wp .AND. l <= SIZE(x_start) )
	345	l = l + 1
	346	ENDDO
	347	num_leg = l-1
[1957]	348	!
[4497]	349	!-- Check for proper parameter settings
	350	CALL flight_check_parameters
[1957]	351	!
[4497]	352	!-- Allocate and initialize logical array for flight pattern
	353	ALLOCATE( cyclic_leg(1:num_leg) )
[1957]	354	!
[4497]	355	!-- Initialize flags for cyclic/return legs
	356	DO l = 1, num_leg
	357	cyclic_leg(l) = MERGE( .TRUE., .FALSE., TRIM( leg_mode(l) ) == 'cyclic' )
	358	ENDDO
[1957]	359	!
[4497]	360	!-- Allocate and initialize arraxs for flight position and speed. In case of restart runs these data
	361	!-- are read by the routine read_flight_restart_data instead.
	362	IF ( TRIM( initializing_actions ) /= 'read_restart_data' ) THEN
	363
	364	ALLOCATE( x_pos(1:num_leg), y_pos(1:num_leg ), z_pos(1:num_leg) )
[1957]	365	!
[4497]	366	!-- Inititalize x-, y-, and z-positions with initial start position
	367	x_pos(1:num_leg) = x_start(1:num_leg)
	368	y_pos(1:num_leg) = y_start(1:num_leg)
	369	z_pos(1:num_leg) = flight_level(1:num_leg)
[1957]	370	!
[4497]	371	!-- Allocate arrays for flight-speed components
	372	ALLOCATE( u_agl(1:num_leg), &
	373	v_agl(1:num_leg), &
	374	w_agl(1:num_leg) )
[1957]	375	!
[4497]	376	!-- Inititalize u-, v- and w-component.
	377	DO l = 1, num_leg
[1957]	378	!
[4497]	379	!-- In case of return-legs, the flight direction, i.e. the horizontal flight-speed components,
	380	!-- are derived from the given start/end positions.
	381	IF ( .NOT. cyclic_leg(l) ) THEN
	382	distance = SQRT( ( x_end(l) - x_start(l) )2 + ( y_end(l) - y_start(l) )2 )
	383	u_agl(l) = speed_agl(l) * ( x_end(l) - x_start(l) ) / distance
	384	v_agl(l) = speed_agl(l) * ( y_end(l) - y_start(l) ) / distance
	385	w_agl(l) = rate_of_climb(l)
[1957]	386	!
[4497]	387	!-- In case of cyclic-legs, flight direction is directly derived from the given flight angle.
	388	ELSE
	389	u_agl(l) = speed_agl(l) * COS( flight_angle(l) * pi / 180.0_wp )
	390	v_agl(l) = speed_agl(l) * SIN( flight_angle(l) * pi / 180.0_wp )
	391	w_agl(l) = rate_of_climb(l)
	392	ENDIF
[1957]	393
[4497]	394	ENDDO
	395
	396	ENDIF
[1957]	397	!
[4497]	398	!-- Initialized data output
	399	CALL flight_init_output
[1957]	400	!
[4497]	401	!-- Allocate array required for user-defined quantities if necessary.
	402	IF ( num_var_fl_user > 0 ) ALLOCATE( var_u(nzb:nzt+1,nysg:nyng,nxlg:nxrg) )
[1957]	403	!
[4497]	404	!-- Allocate and initialize arrays containing the measured data
	405	ALLOCATE( sensor_l(1:num_var_fl,1:num_leg) )
	406	ALLOCATE( sensor(1:num_var_fl,1:num_leg) )
	407	sensor_l = 0.0_wp
	408	sensor = 0.0_wp
[1957]	409
[4497]	410	IF ( debug_output ) CALL debug_message( 'flight_init', 'end' )
[3885]	411
[4497]	412	END SUBROUTINE flight_init
	413
	414
	415	!--------------------------------------------------------------------------------------------------!
[1957]	416	! Description:
	417	! ------------
	418	!> Initialization of output-variable names and units.
[4497]	419	!--------------------------------------------------------------------------------------------------!
	420	SUBROUTINE flight_init_output
[3274]	421
[4497]	422	USE control_parameters, &
	423	ONLY: cloud_droplets, &
	424	humidity, &
	425	neutral, &
	426	passive_scalar
[3274]	427
[4497]	428	USE bulk_cloud_model_mod, &
	429	ONLY: bulk_cloud_model
[1957]	430
[4497]	431	USE netcdf_interface
	432
	433	IMPLICIT NONE
	434
	435	CHARACTER(LEN=10) :: label_leg !< dummy argument to convert integer to string
	436
	437	INTEGER(iwp) :: i !< loop variable
	438	INTEGER(iwp) :: id_pt !< identifyer for labeling
	439	INTEGER(iwp) :: id_q !< identifyer for labeling
	440	INTEGER(iwp) :: id_ql !< identifyer for labeling
	441	INTEGER(iwp) :: id_s !< identifyer for labeling
	442	INTEGER(iwp) :: id_u = 1 !< identifyer for labeling
	443	INTEGER(iwp) :: id_v = 2 !< identifyer for labeling
	444	INTEGER(iwp) :: id_w = 3 !< identifyer for labeling
	445	INTEGER(iwp) :: k !< index variable
	446
	447	LOGICAL :: init = .TRUE. !< flag to distiquish calls of user_init_flight
[1957]	448	!
[4497]	449	!-- Define output quanities, at least three variables are measured (u,v,w)
	450	num_var_fl = 3
	451	IF ( .NOT. neutral ) THEN
	452	num_var_fl = num_var_fl + 1
	453	id_pt = num_var_fl
	454	ENDIF
	455	IF ( humidity ) THEN
	456	num_var_fl = num_var_fl + 1
	457	id_q = num_var_fl
	458	ENDIF
	459	IF ( bulk_cloud_model .OR. cloud_droplets ) THEN
	460	num_var_fl = num_var_fl + 1
	461	id_ql = num_var_fl
	462	ENDIF
	463	IF ( passive_scalar ) THEN
	464	num_var_fl = num_var_fl + 1
	465	id_s = num_var_fl
	466	ENDIF
[1957]	467	!
[4497]	468	!-- Write output strings for dimensions x, y, z
	469	DO l=1, num_leg
[1957]	470
[4497]	471	IF ( l < 10 ) WRITE( label_leg, '(I1)' ) l
	472	IF ( l >= 10 .AND. l < 100 ) WRITE( label_leg, '(I2)' ) l
	473	IF ( l >= 100 .AND. l < 1000 ) WRITE( label_leg, '(I3)' ) l
[1957]	474
[4497]	475	dofl_dim_label_x(l) = 'x_' // TRIM( label_leg )
	476	dofl_dim_label_y(l) = 'y_' // TRIM( label_leg )
	477	dofl_dim_label_z(l) = 'z_' // TRIM( label_leg )
[1957]	478
[4497]	479	ENDDO
	480
[1957]	481	!
[4497]	482	!-- Call user routine to initialize further variables
	483	CALL user_init_flight( init )
[1957]	484	!
[4497]	485	!-- Write output labels and units for the quanities
	486	k = 1
	487	DO l=1, num_leg
[1957]	488
[4497]	489	IF ( l < 10 ) WRITE( label_leg, '(I1)' ) l
	490	IF ( l >= 10 .AND. l < 100 ) WRITE( label_leg, '(I2)' ) l
	491	IF ( l >= 100 .AND. l < 1000 ) WRITE( label_leg, '(I3)' ) l
	492
	493	label_leg = 'leg_' // TRIM(label_leg)
	494	DO i=1, num_var_fl
	495
	496	IF ( i == id_u ) THEN
	497	dofl_label(k) = TRIM( label_leg ) // '_u'
	498	dofl_unit(k) = 'm/s'
	499	k = k + 1
	500	ELSEIF ( i == id_v ) THEN
	501	dofl_label(k) = TRIM( label_leg ) // '_v'
	502	dofl_unit(k) = 'm/s'
	503	k = k + 1
	504	ELSEIF ( i == id_w ) THEN
	505	dofl_label(k) = TRIM( label_leg ) // '_w'
	506	dofl_unit(k) = 'm/s'
	507	k = k + 1
	508	ELSEIF ( i == id_pt ) THEN
	509	dofl_label(k) = TRIM( label_leg ) // '_theta'
	510	dofl_unit(k) = 'K'
	511	k = k + 1
	512	ELSEIF ( i == id_q ) THEN
	513	dofl_label(k) = TRIM( label_leg ) // '_q'
	514	dofl_unit(k) = 'kg/kg'
	515	k = k + 1
	516	ELSEIF ( i == id_ql ) THEN
	517	dofl_label(k) = TRIM( label_leg ) // '_ql'
	518	dofl_unit(k) = 'kg/kg'
	519	k = k + 1
	520	ELSEIF ( i == id_s ) THEN
	521	dofl_label(k) = TRIM( label_leg ) // '_s'
	522	dofl_unit(k) = 'kg/kg'
	523	k = k + 1
	524	ENDIF
	525	ENDDO
	526
	527	DO i=1, num_var_fl_user
	528	CALL user_init_flight( init, k, i, label_leg )
	529	ENDDO
	530
	531	ENDDO
[1957]	532	!
[4497]	533	!-- Finally, set the total number of flight-output quantities.
	534	num_var_fl = num_var_fl + num_var_fl_user
[1957]	535
[4497]	536	END SUBROUTINE flight_init_output
	537
	538	!--------------------------------------------------------------------------------------------------!
[1957]	539	! Description:
	540	! ------------
[4497]	541	!> This routine calculates the current flight positions and calls the respective interpolation
	542	!> routine to measure the data at the current flight position.
	543	!--------------------------------------------------------------------------------------------------!
	544	SUBROUTINE flight_measurement
[1957]	545
[4497]	546	USE arrays_3d, &
	547	ONLY: ddzu, &
	548	ddzw, &
	549	pt, &
	550	q, &
	551	ql, &
	552	s, &
	553	u, &
	554	v, &
	555	w, &
	556	zu, &
	557	zw
[1957]	558
[4497]	559	USE control_parameters, &
	560	ONLY: cloud_droplets, &
	561	dt_3d, &
	562	humidity, &
	563	neutral, &
	564	passive_scalar, &
[4541]	565	time_since_reference_point
[1957]	566
[4497]	567	USE cpulog, &
	568	ONLY: cpu_log, &
	569	log_point
[1957]	570
[4497]	571	USE grid_variables, &
	572	ONLY: ddx, &
	573	ddy, &
	574	dx, &
	575	dy
[1957]	576
[4497]	577	USE indices, &
	578	ONLY: nx, &
	579	nxl, &
	580	nxr, &
	581	ny, &
	582	nys, &
	583	nyn
[3274]	584
[4497]	585	USE bulk_cloud_model_mod, &
	586	ONLY: bulk_cloud_model
[1957]	587
[4497]	588	USE pegrid
[1957]	589
[4497]	590	IMPLICIT NONE
[1957]	591
[4497]	592	INTEGER(iwp) :: i !< index of current grid box along x
	593	INTEGER(iwp) :: j !< index of current grid box along y
	594	INTEGER(iwp) :: n !< loop variable for number of user-defined output quantities
[1957]	595
[4497]	596	LOGICAL :: on_pe !< flag to check if current flight position is on current PE
	597
	598	REAL(wp) :: x !< distance between left edge of current grid box and flight position
	599	REAL(wp) :: y !< distance between south edge of current grid box and flight position
	600
	601	CALL cpu_log( log_point(65), 'flight_measurement', 'start' )
[1957]	602	!
[4497]	603	!-- Perform flight measurement if start time is reached.
[4541]	604	IF ( time_since_reference_point >= flight_begin .AND. time_since_reference_point <= flight_end ) THEN
[1957]	605
[4497]	606	sensor_l = 0.0_wp
	607	sensor = 0.0_wp
[1957]	608	!
[4497]	609	!-- Loop over all flight legs
	610	DO l = 1, num_leg
[1957]	611	!
[4497]	612	!-- Update location for each leg
	613	x_pos(l) = x_pos(l) + u_agl(l) * dt_3d
	614	y_pos(l) = y_pos(l) + v_agl(l) * dt_3d
	615	z_pos(l) = z_pos(l) + w_agl(l) * dt_3d
[1957]	616	!
[4497]	617	!-- Check if location must be modified for return legs.
	618	!-- Carry out horizontal reflection if required.
	619	IF ( .NOT. cyclic_leg(l) ) THEN
[4004]	620
[4497]	621	IF ( x_start(l) <= x_end(l) ) THEN
[1957]	622	!
[4497]	623	!-- Outward flight, i.e. from start to end
	624	IF ( u_agl(l) >= 0.0_wp .AND. x_pos(l) > x_end(l) ) THEN
	625	x_pos(l) = 2.0_wp * x_end(l) - x_pos(l)
	626	u_agl(l) = - u_agl(l)
[1957]	627	!
[4497]	628	!-- Return flight, i.e. from end to start
	629	ELSEIF ( u_agl(l) < 0.0_wp .AND. x_pos(l) < x_start(l) ) THEN
	630	x_pos(l) = 2.0_wp * x_start(l) - x_pos(l)
	631	u_agl(l) = - u_agl(l)
[1957]	632	ENDIF
[4497]	633	ELSE
[1957]	634	!
[4497]	635	!-- Outward flight, i.e. from start to end
	636	IF ( u_agl(l) < 0.0_wp .AND. x_pos(l) < x_end(l) ) THEN
	637	x_pos(l) = 2.0_wp * x_end(l) - x_pos(l)
	638	u_agl(l) = - u_agl(l)
[1957]	639	!
[4497]	640	!-- Return flight, i.e. from end to start
	641	ELSEIF ( u_agl(l) >= 0.0_wp .AND. x_pos(l) > x_start(l) ) THEN
	642	x_pos(l) = 2.0_wp * x_start(l) - x_pos(l)
	643	u_agl(l) = - u_agl(l)
[1957]	644	ENDIF
[4497]	645	ENDIF
	646
	647	IF ( y_start(l) <= y_end(l) ) THEN
[1957]	648	!
[4497]	649	!-- Outward flight, i.e. from start to end
	650	IF ( v_agl(l) >= 0.0_wp .AND. y_pos(l) > y_end(l) ) THEN
	651	y_pos(l) = 2.0_wp * y_end(l) - y_pos(l)
	652	v_agl(l) = - v_agl(l)
[1957]	653	!
[4497]	654	!-- Return flight, i.e. from end to start
	655	ELSEIF ( v_agl(l) < 0.0_wp .AND. y_pos(l) < y_start(l) ) THEN
	656	y_pos(l) = 2.0_wp * y_start(l) - y_pos(l)
	657	v_agl(l) = - v_agl(l)
	658	ENDIF
	659	ELSE
[1957]	660	!
[4497]	661	!-- Outward flight, i.e. from start to end
	662	IF ( v_agl(l) < 0.0_wp .AND. y_pos(l) < y_end(l) ) THEN
	663	y_pos(l) = 2.0_wp * y_end(l) - y_pos(l)
	664	v_agl(l) = - v_agl(l)
[1957]	665	!
[4497]	666	!-- Return flight, i.e. from end to start
	667	ELSEIF ( v_agl(l) >= 0.0_wp .AND. y_pos(l) > y_start(l) ) THEN
	668	y_pos(l) = 2.0_wp * y_start(l) - y_pos(l)
	669	v_agl(l) = - v_agl(l)
[1957]	670	ENDIF
	671	ENDIF
	672	!
[4497]	673	!-- Check if flight position is outside the model domain and apply cyclic conditions if required
	674	ELSEIF ( cyclic_leg(l) ) THEN
[1957]	675	!
[4497]	676	!-- Check if aircraft leaves the model domain at the right boundary
	677	IF ( ( flight_angle(l) >= 0.0_wp .AND. &
	678	flight_angle(l) <= 90.0_wp ) .OR. &
	679	( flight_angle(l) >= 270.0_wp .AND. &
	680	flight_angle(l) <= 360.0_wp ) ) THEN
	681	IF ( x_pos(l) >= ( nx + 0.5_wp ) * dx ) &
	682	x_pos(l) = x_pos(l) - ( nx + 1 ) * dx
[1957]	683	!
[4497]	684	!-- Check if aircraft leaves the model domain at the left boundary
	685	ELSEIF ( flight_angle(l) > 90.0_wp .AND. flight_angle(l) < 270.0_wp ) THEN
	686	IF ( x_pos(l) < -0.5_wp * dx ) &
	687	x_pos(l) = ( nx + 1 ) * dx + x_pos(l)
	688	ENDIF
[1957]	689	!
[4497]	690	!-- Check if aircraft leaves the model domain at the north boundary
	691	IF ( flight_angle(l) >= 0.0_wp .AND. flight_angle(l) <= 180.0_wp ) THEN
	692	IF ( y_pos(l) >= ( ny + 0.5_wp ) * dy ) &
	693	y_pos(l) = y_pos(l) - ( ny + 1 ) * dy
[1957]	694	!
[4497]	695	!-- Check if aircraft leaves the model domain at the south boundary
	696	ELSEIF ( flight_angle(l) > 180.0_wp .AND. flight_angle(l) < 360.0_wp ) THEN
	697	IF ( y_pos(l) < -0.5_wp * dy ) &
	698	y_pos(l) = ( ny + 1 ) * dy + y_pos(l)
	699	ENDIF
[1957]	700
[4497]	701	ENDIF
	702	!
	703	!-- Check if maximum elevation change is already reached. If required reflect vertically.
	704	IF ( rate_of_climb(l) /= 0.0_wp ) THEN
	705	!
	706	!-- First check if aircraft is too high
	707	IF ( w_agl(l) > 0.0_wp .AND. z_pos(l) - flight_level(l) > max_elev_change(l) ) THEN
	708	z_pos(l) = 2.0_wp * ( flight_level(l) + max_elev_change(l) ) - z_pos(l)
	709	w_agl(l) = - w_agl(l)
	710	!
	711	!-- Check if aircraft is too low
	712	ELSEIF ( w_agl(l) < 0.0_wp .AND. z_pos(l) < flight_level(l) ) THEN
	713	z_pos(l) = 2.0_wp * flight_level(l) - z_pos(l)
	714	w_agl(l) = - w_agl(l)
	715	ENDIF
[1957]	716
[4497]	717	ENDIF
[1957]	718	!
[4497]	719	!-- Determine grid indices for flight position along x- and y-direction. Please note, there is
	720	!-- a special treatment for the index along z-direction, which is due to vertical grid stretching.
	721	i = ( x_pos(l) + 0.5_wp * dx ) * ddx
	722	j = ( y_pos(l) + 0.5_wp * dy ) * ddy
[1957]	723	!
[4497]	724	!-- Check if indices are on current PE
	725	on_pe = ( i >= nxl .AND. i <= nxr .AND. j >= nys .AND. j <= nyn )
	726
	727	IF ( on_pe ) THEN
	728
	729	var_index = 1
[1957]	730	!
[4497]	731	!-- Recalculate indices, as u is shifted by -0.5*dx.
	732	i = x_pos(l) * ddx
	733	j = ( y_pos(l) + 0.5_wp * dy ) * ddy
[1957]	734	!
[4497]	735	!-- Calculate distance from left and south grid-box edges.
	736	x = x_pos(l) - ( 0.5_wp - i ) * dx
	737	y = y_pos(l) - j * dy
	738	!
	739	!-- Interpolate u-component onto current flight position.
	740	CALL interpolate_xyz( u, zu, ddzu, 1.0_wp, x, y, var_index, j, i )
	741	var_index = var_index + 1
	742	!
	743	!-- Recalculate indices, as v is shifted by -0.5*dy.
	744	i = ( x_pos(l) + 0.5_wp * dx ) * ddx
	745	j = y_pos(l) * ddy
[1957]	746
[4497]	747	x = x_pos(l) - i * dx
	748	y = y_pos(l) - ( 0.5_wp - j ) * dy
	749	CALL interpolate_xyz( v, zu, ddzu, 1.0_wp, x, y, var_index, j, i )
	750	var_index = var_index + 1
[1957]	751	!
[4497]	752	!-- Interpolate w and scalar quantities. Recalculate indices.
	753	i = ( x_pos(l) + 0.5_wp * dx ) * ddx
	754	j = ( y_pos(l) + 0.5_wp * dy ) * ddy
	755	x = x_pos(l) - i * dx
	756	y = y_pos(l) - j * dy
[1957]	757	!
[4497]	758	!-- Interpolate w-velocity component.
	759	CALL interpolate_xyz( w, zw, ddzw, 0.0_wp, x, y, var_index, j, i )
	760	var_index = var_index + 1
	761	!
	762	!-- Potential temerature
	763	IF ( .NOT. neutral ) THEN
	764	CALL interpolate_xyz( pt, zu, ddzu, 1.0_wp, x, y, var_index, j, i )
[1957]	765	var_index = var_index + 1
[4497]	766	ENDIF
[1957]	767	!
[4497]	768	!-- Humidity
	769	IF ( humidity ) THEN
	770	CALL interpolate_xyz( q, zu, ddzu, 1.0_wp, x, y, var_index, j, i )
	771	var_index = var_index + 1
	772	ENDIF
[1957]	773	!
[4497]	774	!-- Liquid water content
	775	IF ( bulk_cloud_model .OR. cloud_droplets ) THEN
	776	CALL interpolate_xyz( ql, zu, ddzu, 1.0_wp, x, y, var_index, j, i )
	777	var_index = var_index + 1
	778	ENDIF
[1957]	779	!
[4497]	780	!-- Passive scalar
	781	IF ( passive_scalar ) THEN
	782	CALL interpolate_xyz( s, zu, ddzu, 1.0_wp, x, y, var_index, j, i )
	783	var_index = var_index + 1
	784	ENDIF
[1957]	785	!
[4497]	786	!-- Treat user-defined variables if required
	787	DO n = 1, num_var_fl_user
	788	CALL user_flight( var_u, n )
	789	CALL interpolate_xyz( var_u, zu, ddzu, 1.0_wp, x, y, var_index, j, i )
	790	var_index = var_index + 1
	791	ENDDO
	792	ENDIF
[1957]	793
[4497]	794	ENDDO
[1957]	795	!
[4497]	796	!-- Write local data on global array.
[1957]	797	#if defined( __parallel )
[4497]	798	CALL MPI_ALLREDUCE( sensor_l(1,1), sensor(1,1), num_var_fl * num_leg, MPI_REAL, MPI_SUM, &
	799	comm2d, ierr )
[1957]	800	#else
[4497]	801	sensor = sensor_l
[1957]	802	#endif
[4497]	803	ENDIF
[1957]	804
[4497]	805	CALL cpu_log( log_point(65), 'flight_measurement', 'stop' )
[1957]	806
[4497]	807	END SUBROUTINE flight_measurement
	808
	809	!--------------------------------------------------------------------------------------------------!
[1957]	810	! Description:
	811	! ------------
[4497]	812	!> This subroutine bi-linearly interpolates the respective data onto the current flight position.
	813	!--------------------------------------------------------------------------------------------------!
	814	SUBROUTINE interpolate_xyz( var, z_uw, ddz_uw, fac, x, y, var_ind, j, i )
[1957]	815
[4497]	816	USE control_parameters, &
	817	ONLY: dz, &
	818	dz_stretch_level_start
[1957]	819
[4497]	820	USE grid_variables, &
	821	ONLY: dx, &
	822	dy
[1957]	823
[4497]	824	USE indices, &
	825	ONLY: nzb, &
	826	nzt, &
	827	nxlg, &
	828	nxrg, &
	829	nysg, &
	830	nyng
[1957]	831
[4497]	832	IMPLICIT NONE
[1957]	833
[4497]	834	INTEGER(iwp) :: i !< index along x
	835	INTEGER(iwp) :: j !< index along y
	836	INTEGER(iwp) :: k !< index along z
	837	INTEGER(iwp) :: k1 !< dummy variable
	838	INTEGER(iwp) :: var_ind !< index variable for output quantity
[1957]	839
[4497]	840	REAL(wp) :: aa !< dummy argument for horizontal interpolation
	841	REAL(wp) :: bb !< dummy argument for horizontal interpolation
	842	REAL(wp) :: cc !< dummy argument for horizontal interpolation
	843	REAL(wp) :: dd !< dummy argument for horizontal interpolation
	844	REAL(wp) :: gg !< dummy argument for horizontal interpolation
	845	REAL(wp) :: fac !< flag to indentify if quantity is on zu or zw level
	846	REAL(wp) :: var_int !< horizontal interpolated variable at current position
	847	REAL(wp) :: var_int_l !< horizontal interpolated variable at k-level
	848	REAL(wp) :: var_int_u !< horizontal interpolated variable at (k+1)-level
	849	REAL(wp) :: x !< distance between left edge of current grid box and flight position
	850	REAL(wp) :: y !< distance between south edge of current grid box and flight position
	851
	852	REAL(wp), DIMENSION(1:nzt+1) :: ddz_uw !< inverse vertical grid spacing
	853	REAL(wp), DIMENSION(nzb:nzt+1) :: z_uw !< height level
	854
	855	REAL(wp), DIMENSION(nzb:nzt+1,nysg:nyng,nxlg:nxrg) :: var !< treated quantity
[1957]	856	!
[4497]	857	!-- Calculate interpolation coefficients
	858	aa = x2 + y2
	859	bb = ( dx - x )2 + y2
	860	cc = x2 + ( dy - y )2
	861	dd = ( dx - x )2 + ( dy - y )2
	862	gg = aa + bb + cc + dd
[1957]	863	!
[4497]	864	!-- Obtain vertical index. Special treatment for grid index along z-direction if flight position is
	865	!-- above the vertical grid-stretching level. fac=1 if variable is on scalar grid level, fac=0 for
	866	!-- w-component.
	867	IF ( z_pos(l) < dz_stretch_level_start(1) ) THEN
	868	k = ( z_pos(l) + fac * 0.5_wp * dz(1) ) / dz(1)
	869	ELSE
[1957]	870	!
[4497]	871	!-- Search for k-index
	872	DO k1 = nzb, nzt
	873	IF ( z_pos(l) >= z_uw(k1) .AND. z_pos(l) < z_uw(k1+1) ) THEN
	874	k = k1
	875	EXIT
	876	ENDIF
	877	ENDDO
	878	ENDIF
[1957]	879	!
[4497]	880	!-- (x,y)-interpolation at k-level
	881	var_int_l = ( ( gg - aa ) * var(k,j,i) + &
	882	( gg - bb ) * var(k,j,i+1) + &
	883	( gg - cc ) * var(k,j+1,i) + &
	884	( gg - dd ) * var(k,j+1,i+1) &
	885	) / ( 3.0_wp * gg )
[1957]	886	!
[4497]	887	!-- (x,y)-interpolation on (k+1)-level
	888	var_int_u = ( ( gg - aa ) * var(k+1,j,i) + &
	889	( gg - bb ) * var(k+1,j,i+1) + &
	890	( gg - cc ) * var(k+1,j+1,i) + &
	891	( gg - dd ) * var(k+1,j+1,i+1) &
	892	) / ( 3.0_wp * gg )
[1957]	893	!
[4497]	894	!-- z-interpolation onto current flight postion
	895	var_int = var_int_l + ( z_pos(l) - z_uw(k) ) * ddz_uw(k+1) * (var_int_u - var_int_l )
[1957]	896	!
[4497]	897	!-- Store on local data array
	898	sensor_l(var_ind,l) = var_int
[1957]	899
[4497]	900	END SUBROUTINE interpolate_xyz
[1957]	901
[4497]	902	!--------------------------------------------------------------------------------------------------!
[1957]	903	! Description:
	904	! ------------
	905	!> Perform parameter checks.
[4497]	906	!--------------------------------------------------------------------------------------------------!
	907	SUBROUTINE flight_check_parameters
[1957]	908
[4497]	909	USE arrays_3d, &
	910	ONLY: zu
[1957]	911
[4497]	912	USE control_parameters, &
	913	ONLY: bc_lr_cyc, &
	914	bc_ns_cyc, &
	915	message_string
[1957]	916
[4497]	917	USE grid_variables, &
	918	ONLY: dx, &
	919	dy
	920
	921	USE indices, &
	922	ONLY: nx, &
	923	ny, &
	924	nz
	925
	926	USE netcdf_interface, &
	927	ONLY: netcdf_data_format
	928
	929	IMPLICIT NONE
	930
[1957]	931	!
[4497]	932	!-- Check if start positions are properly set.
	933	DO l = 1, num_leg
	934	IF ( x_start(l) < 0.0_wp .OR. x_start(l) > ( nx + 1 ) * dx ) THEN
	935	message_string = 'Start x position is outside the model domain'
	936	CALL message( 'flight_check_parameters', 'PA0431', 1, 2, 0, 6, 0 )
	937	ENDIF
	938	IF ( y_start(l) < 0.0_wp .OR. y_start(l) > ( ny + 1 ) * dy ) THEN
	939	message_string = 'Start y position is outside the model domain'
	940	CALL message( 'flight_check_parameters', 'PA0432', 1, 2, 0, 6, 0 )
	941	ENDIF
[1957]	942
[4497]	943	ENDDO
[1957]	944	!
[4497]	945	!-- Check for leg mode
	946	DO l = 1, num_leg
[1957]	947	!
[4497]	948	!-- Check if leg mode matches the overall lateral model boundary conditions.
	949	IF ( TRIM( leg_mode(l) ) == 'cyclic' ) THEN
	950	IF ( .NOT. bc_lr_cyc .OR. .NOT. bc_ns_cyc ) THEN
	951	message_string = 'Cyclic flight leg does not match lateral boundary condition'
	952	CALL message( 'flight_check_parameters', 'PA0433', 1, 2, 0, 6, 0 )
	953	ENDIF
[1957]	954	!
[4497]	955	!-- Check if end-positions are inside the model domain in case of return-legs.
	956	ELSEIF ( TRIM( leg_mode(l) ) == 'return' ) THEN
	957	IF ( x_end(l) > ( nx + 1 ) * dx .OR. y_end(l) > ( ny + 1 ) * dx ) THEN
	958	message_string = 'Flight leg or parts of it are outside the model domain'
	959	CALL message( 'flight_check_parameters', 'PA0434', 1, 2, 0, 6, 0 )
[1957]	960	ENDIF
[4497]	961	ELSE
	962	message_string = 'Unknown flight mode'
	963	CALL message( 'flight_check_parameters', 'PA0435', 1, 2, 0, 6, 0 )
	964	ENDIF
[1957]	965
[4497]	966	ENDDO
[1957]	967	!
[4497]	968	!-- Check if given flight object remains inside model domain if a rate of climb / descent is
	969	!-- prescribed.
	970	DO l = 1, num_leg
	971	IF ( flight_level(l) + max_elev_change(l) > zu(nz) .OR. &
	972	flight_level(l) + max_elev_change(l) <= 0.0_wp ) THEN
	973	message_string = 'Flight level is outside the model domain '
	974	CALL message( 'flight_check_parameters', 'PA0438', 1, 2, 0, 6, 0 )
	975	ENDIF
	976	ENDDO
[1957]	977	!
[4497]	978	!-- Check for appropriate NetCDF format. Definition of more than one unlimited dimension is
	979	!-- unfortunately only possible with NetCDF4/HDF5.
	980	IF ( netcdf_data_format <= 2 ) THEN
	981	message_string = 'netcdf_data_format must be > 2'
	982	CALL message( 'flight_check_parameters', 'PA0439', 1, 2, 0, 6, 0 )
	983	ENDIF
[1957]	984
	985
[4497]	986	END SUBROUTINE flight_check_parameters
[2576]	987
[4497]	988
	989	!--------------------------------------------------------------------------------------------------!
[2576]	990	! Description:
	991	! ------------
[4495]	992	!> Read module-specific global restart data (Fortran binary format).
[4497]	993	!--------------------------------------------------------------------------------------------------!
	994	SUBROUTINE flight_rrd_global_ftn( found )
[2576]	995
	996
[4497]	997	USE control_parameters, &
	998	ONLY: length, &
	999	restart_string
[2576]	1000
[1957]	1001
[4497]	1002	IMPLICIT NONE
[2894]	1003
[4497]	1004	LOGICAL, INTENT(OUT) :: found !< flag indicating if a variable string is found
[2894]	1005
	1006
[4497]	1007	found = .TRUE.
[2894]	1008
	1009
[4497]	1010	SELECT CASE ( restart_string(1:length) )
[1957]	1011
[4497]	1012	CASE ( 'u_agl' )
	1013	IF ( .NOT. ALLOCATED( u_agl ) ) ALLOCATE( u_agl(1:num_leg) )
	1014	READ ( 13 ) u_agl
	1015	CASE ( 'v_agl' )
	1016	IF ( .NOT. ALLOCATED( v_agl ) ) ALLOCATE( v_agl(1:num_leg) )
	1017	READ ( 13 ) v_agl
	1018	CASE ( 'w_agl' )
	1019	IF ( .NOT. ALLOCATED( w_agl ) ) ALLOCATE( w_agl(1:num_leg) )
	1020	READ ( 13 ) w_agl
	1021	CASE ( 'x_pos' )
	1022	IF ( .NOT. ALLOCATED( x_pos ) ) ALLOCATE( x_pos(1:num_leg) )
	1023	READ ( 13 ) x_pos
	1024	CASE ( 'y_pos' )
	1025	IF ( .NOT. ALLOCATED( y_pos ) ) ALLOCATE( y_pos(1:num_leg) )
	1026	READ ( 13 ) y_pos
	1027	CASE ( 'z_pos' )
	1028	IF ( .NOT. ALLOCATED( z_pos ) ) ALLOCATE( z_pos(1:num_leg) )
	1029	READ ( 13 ) z_pos
[2894]	1030
[4497]	1031	CASE DEFAULT
[4495]	1032
[4497]	1033	found = .FALSE.
[4495]	1034
[4497]	1035	END SELECT
	1036
	1037
	1038	END SUBROUTINE flight_rrd_global_ftn
	1039
	1040
	1041
[4495]	1042	!------------------------------------------------------------------------------!
	1043	! Description:
	1044	! ------------
	1045	!> Read module-specific global restart data (MPI-IO).
	1046	!------------------------------------------------------------------------------!
[4497]	1047	SUBROUTINE flight_rrd_global_mpi
[4495]	1048
	1049
[4497]	1050	IMPLICIT NONE
[4495]	1051
[4497]	1052	LOGICAL :: array_found !< flag indicating if respective array is found in restart file
[4495]	1053
	1054
[4497]	1055	CALL rd_mpi_io_check_array( 'u_agl', found = array_found )
	1056	IF ( array_found) THEN
	1057	IF ( .NOT. ALLOCATED( u_agl ) ) ALLOCATE( u_agl(1:num_leg) )
	1058	CALL rrd_mpi_io_global_array( 'u_agl', u_agl )
	1059	ENDIF
	1060	CALL rd_mpi_io_check_array( 'v_agl', found = array_found )
	1061	IF ( array_found) THEN
	1062	IF ( .NOT. ALLOCATED( v_agl ) ) ALLOCATE( v_agl(1:num_leg) )
	1063	CALL rrd_mpi_io_global_array( 'v_agl', v_agl )
	1064	ENDIF
	1065	CALL rd_mpi_io_check_array( 'w_agl', found = array_found )
	1066	IF ( array_found) THEN
	1067	IF ( .NOT. ALLOCATED( w_agl ) ) ALLOCATE( w_agl(1:num_leg) )
	1068	CALL rrd_mpi_io_global_array( 'w_agl', w_agl )
	1069	ENDIF
	1070	CALL rd_mpi_io_check_array( 'x_pos', found = array_found )
	1071	IF ( array_found) THEN
	1072	IF ( .NOT. ALLOCATED( x_pos ) ) ALLOCATE( x_pos(1:num_leg) )
	1073	CALL rrd_mpi_io_global_array( 'x_pos', x_pos )
	1074	ENDIF
	1075	CALL rd_mpi_io_check_array( 'y_pos', found = array_found )
	1076	IF ( array_found) THEN
	1077	IF ( .NOT. ALLOCATED( y_pos ) ) ALLOCATE( y_pos(1:num_leg) )
	1078	CALL rrd_mpi_io_global_array( 'y_pos', y_pos )
	1079	ENDIF
	1080	CALL rd_mpi_io_check_array( 'z_pos', found = array_found )
	1081	IF ( array_found) THEN
	1082	IF ( .NOT. ALLOCATED( z_pos ) ) ALLOCATE( z_pos(1:num_leg) )
	1083	CALL rrd_mpi_io_global_array( 'z_pos', z_pos )
	1084	ENDIF
[4495]	1085
[4497]	1086	END SUBROUTINE flight_rrd_global_mpi
[4495]	1087
[1957]	1088
[4497]	1089	!--------------------------------------------------------------------------------------------------!
[1957]	1090	! Description:
	1091	! ------------
	1092	!> This routine writes the respective restart data.
[4497]	1093	!--------------------------------------------------------------------------------------------------!
	1094	SUBROUTINE flight_wrd_global
[1957]	1095
[2894]	1096
[4497]	1097	IMPLICIT NONE
[2894]	1098
[3182]	1099
[4497]	1100	IF ( TRIM( restart_data_format_output ) == 'fortran_binary' ) THEN
[2894]	1101
[4497]	1102	CALL wrd_write_string( 'u_agl' )
	1103	WRITE ( 14 ) u_agl
[2894]	1104
[4497]	1105	CALL wrd_write_string( 'v_agl' )
	1106	WRITE ( 14 ) v_agl
[2894]	1107
[4497]	1108	CALL wrd_write_string( 'w_agl' )
	1109	WRITE ( 14 ) w_agl
[2894]	1110
[4497]	1111	CALL wrd_write_string( 'x_pos' )
	1112	WRITE ( 14 ) x_pos
[4495]	1113
[4497]	1114	CALL wrd_write_string( 'y_pos' )
	1115	WRITE ( 14 ) y_pos
[4495]	1116
[4497]	1117	CALL wrd_write_string( 'z_pos' )
	1118	WRITE ( 14 ) z_pos
[4495]	1119
[4535]	1120	ELSEIF ( restart_data_format_output(1:3) == 'mpi' ) THEN
[4495]	1121
[4497]	1122	CALL wrd_mpi_io_global_array( 'u_agl', u_agl )
	1123	CALL wrd_mpi_io_global_array( 'v_agl', v_agl )
	1124	CALL wrd_mpi_io_global_array( 'w_agl', w_agl )
	1125	CALL wrd_mpi_io_global_array( 'x_pos', x_pos )
	1126	CALL wrd_mpi_io_global_array( 'y_pos', y_pos )
	1127	CALL wrd_mpi_io_global_array( 'z_pos', z_pos )
[4495]	1128
[4497]	1129	ENDIF
[1957]	1130
[4497]	1131	END SUBROUTINE flight_wrd_global
	1132
	1133
[1957]	1134	END MODULE flight_mod

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