C This code is taken from "A Guide to the Use of the ITS Irregular C Terrain Model in the Area Prediction Mode," by G.A. Hufford, C A.G. Longley, and W.A. Kissick. It is ITM v1.2.1 from 1982. C provided for historical interest and superceded by newer C versions. Please do not use this for your propagation C predictions. This does not include the 1985 corrections by C Hufford. C C You will likely need a FORTRAN-IV compiler like ifort. While it C compiles under f77 with warnings, results include some NaNs. C After compiling, run without command line arguments and output C will be be printed to stdout. For example, C C ifort -o lr1982 lr1982-f4.f C lr1982 < inputDeck | more C C File inputDeck follows, where of course leading 'C' is removed, C but not leading spaces: C=== inputDeck follows === C 1 CTEST PROBLEM 1, QKAREA C 2 0. 100. 10. 400. 25. C 32 70. C 4 10. 50. 90. 95. C870110 400. 10. 1. 200. C 1 CTEST PROBLEM 2, QKAREA C861 25. C99 C 1 CTEST PROBLEM 4, QKAREA C 31 10. C 57 30. 350. 300. 25. 0.02 C 60000 1200. 5. 1000. C88 C C=== inputDeck ends after required blank line === C C Mike Markowski, mike.ab3ap@gmail.com C Dec 2022 SUBROUTINE LRPROP(D) C COMPUTES AREF, THE REFERENCE VALUE OF RADIO ATTENUATION C VERSION 1.2.1 (AUG 71/MAR 77/APR 79) C OF THE LONGLEY-RICE (1968) MODEL C PRINCIPAL CHANGES- C 1.1. A SIMPLIFICATION OF THE LINE-OF-SIGHT AND SCATTER C ROUTINES C 1.2. A CHANGE IN THE LINE-OF-SIGHT ROUTINE AND IN THE C SUBSEQUENT CALCULATIONS. RESULTS ARE IMPROVED WHEN C ONE OR BOTH ANTENNAS ARE HIGH. C VALID ONLY FOR... C FREQUENCIES BETWEEN 20 MHZ AND 20 GHZ C ANTENNA HEIGHTS BETWEEN 0.5 M AND 3000 M C ELEVATION ANGLES LESS THAN 200 MRAD C COMMON/PROP/KWX,AREF,MDP,DIST,HG(2),WN,DH,ENS,GME,ZGND, X HE(2),DL(2),THE(2) COMPLEX ZGND COMMON/PROPA/DLSA,DX,AEL,AK1,AK2,AED,EMD,AES,EMS,DLS(2),DLA,THA C COMMON/SAVE/SAVA(6),WLOS,WSCAT,DMIN,XAE,SAVB(40) C LOGICAL WLOS,WSCAT C DATA THIRD/0.3333333/ C IF(MDP) 10,32,10 C 10 CONTINUE DO 11 J=1,2 11 DLS(J)=SQRT(2.*HE(J)/GME) DLSA=DLS(1)+DLS(2) DLA=DL(1)+DL(2) THA=AMAX1(THE(1)+THE(2),-DLA*GME) WLOS=.FALSE. WSCAT=.FALSE. C C CHECK PARAMETER RANGES IF(ENS .LT. 250. .OR. ENS .GT. 400.) GO TO 154 IF(GME .LT. 75E-9 .OR. GME .GT. 250E-9) GO TO 154 IF(REAL(ZGND) .LE. ABS(AIMAG(ZGND))) GO TO 154 DO 121 J=1,2 IF(ABS(THE(J)) .GT. 200E-3) GO TO 153 IF(DL(J) .LT. 0.1*DLS(J) .OR. DL(J) .GT. 3.*DLS(J)) X GO TO 153 121 CONTINUE IF(WN .LT. 0.838 .OR. WN .GT. 210.) GO TO 151 DO 122 J=1,2 IF(HG(J) .LT. 1. .OR. HG(J) .GT. 1000.) GO TO 151 122 CONTINUE GO TO 158 153 KWX=MAX0(KWX,3) 151 KWX=MAX0(KWX,1) IF(WN .LT. 0.419 .OR. WN .GT. 420.) GO TO 154 DO 132 J=1,2 IF(HG(J) .LT. 0.5 .OR. HG(J) .GT. 3000.) GO TO 154 132 CONTINUE GO TO 158 154 KWX=4 158 CONTINUE DMIN=ABS(HE(1)-HE(2))/200E-3 C C COEFFICIENTS FOR THE DIFFRACTION RANGE C Q=ADIFF(0.) XAE=(WN*GME**2)**(-THIRD) D3=AMAX1(DLSA,1.3787*XAE+DLA) D4=D3+2.7574*XAE A3=ADIFF(D3) A4=ADIFF(D4) EMD=(A4-A3)/(D4-D3) AED=A3-EMD*D3 C IF(MDP) 33,32,31 31 MDP=0 32 DIST=D IF(DIST .LE. 0.) GO TO 38 33 CONTINUE IF(DIST .GT. 1000E3) KWX=MAX0(KWX,1) IF(DIST .LT. DMIN) KWX=MAX0(KWX,3) IF(DIST .LT. 1E3 .OR. DIST .GT. 2000E3) KWX=4 38 CONTINUE C IF(DIST .GE. DLSA) GO TO 50 C IF(WLOS) GO TO 48 C C COEFFICIENTS FOR THE LINE-OF-SIGHT RANGE C Q=ALOS(0.) D2=DLSA A2=AED+D2*EMD D0=1.908*WN*HE(1)*HE(2) IF(AED .LT. 0.) GO TO 41 D0=AMIN1(D0,0.5*DLA) D1=D0+0.25*(DLA-D0) GO TO 42 41 D1=AMAX1(-AED/EMD,0.25*DLA) 42 A1=ALOS(D1) IF(D0 .GE. D1) GO TO 43 A0=ALOS(D0) Q=ALOG(D2/D0) AK2=AMAX1(0.,((D2-D0)*(A1-A0)-(D1-D0)*(A2-A0))/ X ((D2-D0)*ALOG(D1/D0)-(D1-D0)*Q)) IF(AK2 .GT. 0.) GO TO 44 IF(AED .GE. 0.) GO TO 44 43 AK2=0. AK1=(A2-A1)/(D2-D1) IF(AK1 .GT. 0.) GO TO 46 GO TO 45 44 AK1=(A2-A0-AK2*Q)/(D2-D0) IF(AK1 .GE. 0.) GO TO 46 AK1=0. AK2=DIM(A2,A0)/Q IF(AK2 .GT. 0.) GO TO 46 45 AK1=EMD 46 AEL=A2-AK1*D2-AK2*ALOG(D2) WLOS=.TRUE. 48 IF(DIST .LE. 0.) GO TO 50 AREF=AEL+AK1*DIST+AK2*ALOG(DIST) GO TO 60 C 50 IF(WSCAT) GO TO 58 C C COEFFICIENTS FOR THE SCATTER RANGE C Q=ASCAT(0.) D5=DLA+200E3 D6=D5+200E3 A6=ASCAT(D6) A5=ASCAT(D5) IF(A5 .LT. 1000.) GO TO 51 EMS=EMD AES=AED DX=10E6 GO TO 52 51 EMS=(A6-A5)/200E3 DX=AMAX1(DLSA,DLA+0.3*XAE*ALOG(47.7*WN), X (A5-AED-EMS*D5)/(EMD-EMS)) AES=(EMD-EMS)*DX+AED 52 WSCAT=.TRUE. C 58 IF(DIST .GT. DX) GO TO 59 AREF=AED+EMD*DIST GO TO 60 59 AREF=AES+EMS*DIST C 60 AREF=DIM(AREF,0.) RETURN END FUNCTION ADIFF(D) C THE *DIFFRACTION ATTENUATION* AT DISTANCE D C A CONVEX COMBINATION OF SMOOTH EARTH DIFFRACTION AND C DOUBLE KNIFE-EDGE DIFFRACTION C A CALL WITH D=0 SETS UP INITIAL CONSTANTS C COMMON/PROP/KWX,AREF,MDP,DIST,HG(2),WN,DH,ENS,GME,ZGND, X HE(2),DL(2),THE(2) COMPLEX ZGND COMMON/PROPA/DLSA,DX,AEL,AK1,AK2,AED,EMD,AES,EMS,DLS(2),DLA,THA C COMMON/SAVE/WD1,XD1,AFO,QK,AHT,XHT,SAVE(44) C DATA THIRD/0.3333333/ C IF(D .GT. 0.) GO TO 10 C Q=HG( 1 )*HG(2) QK=HE(1)*HE(2)-Q IF(MDP .LT. 0) Q=Q+10. WD1=SQRT(1.+QK/Q) XD1=DLA+THA/GME Q=(1.-0.5*EXP(-DLSA/50E3))*DH Q=0.78*Q*EXP(-(Q/16.)**0.25) AFO=AMIN1(15.,2.171*ALOG(1.+4.77E-4*HG(1)*HG(2)*WN*Q)) QK=1./CABS(ZGND) AHT=20. XHT=0. DO 1 J=1,2 A=0.5*DL(J)**2/HE(J) WA=(A*WN)**THIRD PK=QK/WA Q=(1.607-PK)*151.0*WA*DL(J)/A XHT=XHT+Q AHT=AHT+FHT(Q,PK) 1 CONTINUE ADIFF=0. GO TO 80 C 10 CONTINUE TH=THA+D*GME DS=D-DLA Q=0.0795775*WN*DS*TH**2 ADIFF=AKNFE(Q*DL(1)/(DS+DL(1)))+AKNFE(Q*DL(2)/(DS+DL(2))) A=DS/TH WA=(A*WN)**THIRD PK=QK/WA Q=(1.607-PK)*151.0*WA*TH+XHT AR=0.05751*Q-4.343*ALOG(Q)-AHT Q=(WD1+XD1/D)*AMIN1(((1.-0.8*EXP(-D/50E3))*DH*WN),6283.2) WD=25.1/(25.1+SQRT(Q)) ADIFF=(AR-ADIFF)*WD+ADIFF+AFO 80 RETURN END FUNCTION ALOS(D) C THE *LINE-OF-SIGHT ATTENUATION* AT DISTANCE D C A CONVEX COMBINATION OF PLANE EARTH FIELDS AND C DIFFRACTED FIELDS C A CALL WITH D=0 SETS UP INITIAL CONSTANTS C COMMON/PROP/KWX,AREF,MDP,DIST,HG(2),WN,DH,ENS,GME,ZGND, X HE(2),DL(2),THE(2) COMPLEX ZGND COMMON/PROPA/DLSA,DX,AEL,AK1,AK2,AED,EMD,AES,EMS,DLS(2),DLA,THA C COMMON/SAVE/WLS,SAVE(49) C COMPLEX R C ABQ(R)=REAL(R)**2+AIMAG(R)**2 C IF(D .GT. 0.) GO TO 10 C WLS=0.021/(0.021+WN*DH/AMAX1(10E3,DLSA)) ALOS=0. GO TO 80 C 10 CONTINUE Q=(1.-0.8*EXP(-D/50E3))*DH S=0.78*Q*EXP(-(Q/16.)**0.25) Q=HE(1)+HE(2) SPS=Q/SQRT(D**2+Q**2) R=(SPS-ZGND)/(SPS+ZGND)*EXP(-WN*S*SPS) Q=ABQ(R) IF(Q .LT. 0.25 .OR. Q .LT. SPS) R=R*SQRT(SPS/Q) ALOS=EMD*D+AED Q=WN*HE(1)*HE(2)*2./D ALOS=(-4.343*ALOG(ABQ(CMPLX(COS(Q),-SIN(Q))+R))-ALOS)*WLS+ALOS C 80 RETURN END FUNCTION ASCAT(D) C THE *SCATTER ATTENUATION* AT DISTANCE D C USES AN APPROXIMATION TO THE METH0DS OF NBS TN101 WITH C CHECKS FOR INADMISSABLE SITUATIONS C FOR PROPER OPERATION, THE LARGER DISTANCE (D=D6) C MUST BE THE FIRST CALLED C A CALL WITH D=0 SETS UP INITIAL CONSTANTS C COMMON/PROP/KWX,AREF,MDP,DIST,HG(2),WN,DH,ENS,GME,ZGND, X HE(2),DL(2),THE(2) COMPLEX ZGND COMMON/PROPA/DLSA,DX,AEL,AK1,AK2,AED,EMD,AES,EMS,DLS(2),DLA,THA C COMMON/SAVE/AD,RR,ETQ,H0S,SAVE(46) C IF(D .GT. 0.) GO TO 10 C AD=DL(1)-DL(2) RR=HE(2)/HE(1) IF(AD) 1,2,2 1 AD=-AD RR=1./RR 2 ETQ=(5.67E-6*ENS-2.32E-3)*ENS+0.031 H0S=-15. ASCAT=0. GO TO 80 C 10 CONTINUE IF(H0S .GT. 15.) GO TO 12 TH=THE(1)+THE(2)+D*GME R2=2.*WN*TH R1=R2*HE(1) R2=R2*HE(2) IF(R1 .GT. 0.2 .OR. R2 .GT. 0.2) GO TO 11 ASCAT=1001. GO TO 80 11 SS=(D-AD)/(D+AD) Q=RR/SS SS=AMAX1(0.1,SS) Q=AMIN1(AMAX1(0.1,Q),10.) Z0=(D-AD)*(D+AD)*TH*0.25/D ET=(ETQ*EXP(-AMIN1(1.7,Z0/8.0E3)**6)+1.)*Z0/1.7556E3 ETT=AMAX1(ET,1.) H0=(H0F(R1,ETT)+H0F(R2,ETT))*0.5 H0=H0+AMIN1(H0,(1.38-ALOG(ETT))*ALOG(SS)*ALOG(Q)*0.49) H0=DIM(H0,0.) IF(ET .LT. 1.) H0=ET*H0+(1.-ET)*4.343*ALOG(((1.+1.4142/R1)* X (1.+1.4142/R2))**2*(R1+R2)/(R1+R2+2.8284)) IF(H0 .LE. 15. .OR. H0S .LT. 0.) GO TO 13 12 H0=H0S 13 H08=H0 TH=THA+D*GME ASCAT=AHD(TH*D)+4.343*ALOG(47.7*WN*TH**4)- X 0.1*(ENS-301.)*EXP(-TH*O/40E3)+H0 80 RETURN END FUNCTION AKNFE(V2) C KNIFE-EDGE DIFFRACTION C THE FRESNEL INTEGRAL AS A FUNCTION OF V**2 C IF(V2 .GT. 5.76) GO TO 2 1 AKNFE=6.02+9.11*SQRT(V2)-1.27*V2 GO TO 8 2 AKNFE=12.953+4.343*ALOG(V2) 8 RETURN END FUNCTION FHT(X,PK) C THE HEIGHT GAIN OVER A SMOOTH SPHERICAL EARTH C TO BE USED IN THE *THREE RADII* METH0D C IF(X .LT. 200.) GO TO 2 FHT=0.05751*X-4.343*ALOG(X) IF(X .GE. 2000.) GO TO 8 W=0.0134*X*EXP(-0.005*X) FHT=(1.-W)*FHT+W*(17.372*ALOG(X)-117.) GO TO 8 2 IF(PK .GT. 1.E-5) GO TO 3 IF(X .GT. 1.) GO TO 4 FHT=-117. GO TO 8 3 W=-ALOG(PK) IF(X*W**3 .GT. 5495.) GO TO 4 FHT=2.5E-5*X**2/PK-8.686*W-15. GO TO 8 4 FHT=17.372*ALOG(X)-117. 8 RETURN END FUNCTION H0F(R,ET) C THE H0 FUNCTION FOR SCATTER FIELDS C DIMENSION A(5),B(5) C DATA A( 1 ) ,A( 2) ,A( 3) ,A( 4) ,A( 5) X / 25., 80.,177.,395.,705./ DATA B(1),B(2),B(3),B(4),B(5) X / 24., 45., 68., 80.,105./ C IT=ET IF(IT) 2,2,1 1 IF(IT-5) 5,4,3 2 IT=1 GO TO 4 3 IT=5 4 Q=0. GO TO 6 5 Q=ET-FLOAT(IT) 6 X=(1./R)**2 H0F=4.343*ALOG((A(IT)*X+B(IT))*X+1.) IF(Q .NE. 0.) X H0F=(1.-Q)*H0F+Q*4.343*ALOG((A(IT+1)*X+B(IT+1))*X+1.) RETURN END FUNCTION AHD(TD) C THE F(TH*D) FUNCTION FOR SCATTER FIELDS C DIMENSION A(3),B(3),C(3) C DATA A(1),A(2),A(3)/133.4,104.6,71.8/ DATA B(1),B(2),B(3)/0.332E-3,0.212E-3,0.157E-3/ DATA C(1),C(2),C(3)/-4.343,-1.086,2.171/ C I=1 IF(TD .LE. 10E3) GO TO 1 I=2 IF(TD .LE. 70E3) GO TO 1 I=3 1 AHD=A(I)+B(I)*TD+C(I)*ALOG(TD) RETURN END FUNCTION AVAR(ZZT,ZZL,ZZC) C QUANTILES OF ATTENUATION RELATIVE TO FREE SPACE C INCLUDES LONG-TERM TIME VARIABILITY, LOCATION VARIABILITY, C AND SITE VARIABILITY C COMMON/PROP/KWX,AREF,MDP,DIST,HG(2),WN,DH,ENS,GME,ZGND, X HE(2),DL(2),THE(2) COMPLEX ZGND COMMON/PROPV/LVAR,SGC,MDVAR,KLIM C COMMON/SAVE/SAVE(13),KDV,WL,WS,DEXA,DE,VMD,VS0,SGL, X SGTM,SGTP,SGTD,TGTD,GM,GP,CV1,CV2,YV1,YV2,YV3, X CSM1,CSM2,YSM1,YSM2,YSM3,CSP1,CSP2,YSP1,YSP2,YSP3,CSD1,ZD, X CFM1,CFM2,CFM3,CFP1,CFP2,CFP3 C DIMENSION BV1(7),BV2(7),XV1(7),XV2(7),XV3(7) DIMENSION BSM1(7),BSM2(7),XSM1(7),XSM2(7),XSM3(7) DIMENSION BSP1(7),BSP2(7),XSP1(7),XSP2(7),XSP3(7) DIMENSION BSD1(7),BZD1(7) DIMENSION BFM1(7),BFM2(7),BFM3(7),BFP1(7),BFP2(7),BFP3(7) C LOGICAL WS,WL C C EQUATOR, CON SUB, MAR SUB, DESERT, CON TMP, MAR LND, MAR SEA C DATA BV1(1), BV1(2), BV1(3), BV1(4), BV1(5), BV1(6), BV1(7) X / -9.67, -0.62, 1.26, -9.21, -0.62, -0.39, 3.15/ DATA BV2(1), BV2(2), BV2(3), BV2(4), BV2(5), BV2(6), BV2(7) X / 12.7, 9.19, 15.5, 9.05, 9.19, 2.86, 857.9/ DATA XV1(1), XV1(2), XV1(3), XV1(4), XV1(5), XV1(6), XV1(7) X /144.9E3,228.9E3,262.6E3, 84.1E3,228.9E3,141.7E3,2222.E3/ DATA XV2(1), XV2(2), XV2(3), XV2(4), XV2(5), XV2(6), XV2(7) X /190.3E3,205.2E3,185.2E3,101.1E3,205.2E3,315.9E3,164.8E3/ DATA XV3(1), XV3(2), XV3(3), XV3(4), XV3(5), XV3(6), XV3(7) X /133.8E3,143.6E3, 99.8E3, 98.6E3,143.6E3,167.4E3,116.3E3/ DATA BSM1(1),BSM1(2),BSM1(3),BSM1(4),BSM1(5),BSM1(6),BSM1(7) X / 2.13, 2.66, 6.11, 1.98, 2.68, 6.86, 8.51/ DATA BSM2(1),BSM2(2),BSM2(3),BSM2(4),BSM2(5),BSM2(6),BSM2(7) X / 159.5, 7.67, 6.65, 13.11, 7.16, 10.38, 169.8/ DATA XSM1(1),XSM1(2),XSM1(3),XSM1(4),XSM1(5),XSM1(6),XSM1(7) X /762.2E3,100.4E3,138.2E3,139.1E3, 93.7E3,187.8E3,609.8E3/ DATA XSM2(1),XSM2(2),XSM2(3),XSM2(4),XSM2(5),XSM2(6),XSM2(7) X /123.6E3,172.5E3,242.2E3,132.7E3,186.8E3,169.6E3,119.9E3/ DATA XSM3(1),XSM3(2),XSM3(3),XSM3(4),XSM3(5),XSM3(6),XSM3(7) X / 94.5E3,136.4E3,178.6E3,193.5E3,133.5E3,108.9E3,106.6E3/ DATA BSP1(1),BSP1(2),BSP1(3),BSP1(4),BSP1(5),BSP1(6),BSP1(7) X / 2.11, 6.87, 10.08, 3.68, 4.75, 8.58, 8.43/ DATA BSP2(1),BSP2(2),BSP2(3),BSP2(4),BSP2(5),BSP2(6),BSP2(7) X / 102.3, 15.53, 9.60, 159.3, 8.12, 13.97, 8.19/ DATA XSP1(1),XSP1(2),XSP1(3),XSP1(4),XSP1(5),XSP1(6),XSP1(7) X /636.9E3,138.7E3,165.3E3,464.4E3, 93.2E3,216.0E3,136.2E3/ DATA XSP2(1),XSP2(2),XSP2(3),XSP2(4),XSP2(5),XSP2(6),XSP2(7) X /134.8E3,143.7E3,225.7E3, 93.1E3,135.9E3,152.0E3,188.5E3/ DATA XSP3(1),XSP3(2),XSP3(3),XSP3(4),XSP3(5),XSP3(6),XSP3(7) X / 95.6E3, 98.6E3,129.7E3, 94.2E3,113.4E3,122.7E3,122.9E3/ DATA BSD1(1),BSD1(2),BSD1(3),BSD1(4),BSD1(5),BSD1(6),BSD1(7) X / 1.224, 0.801, 1.380, 1.000, 1.224, 1.518, 1.518/ DATA BZD1(1),BZD1(2),BZD1(3),BZD1(4),BZD1(5),BZD1(6),BZD1(7) X / 1.282, 2.161, 1.282, 20., 1.282, 1.282, 1.282/ DATA BFM1(1),BFM1(2),BFM1(3),BFM1(4),BFM1(5),BFM1(6),BFM1(7) X / 1., 1., 1., 1., 0.92, 1., 1./ DATA BFM2(1),BFM2(2),BFM2(3),BFM2(4),BFM2(5),BFM2(6),BFM2(7) X / 0., 0., 0., 0., 0 .25, 0., 0./ DATA BFM3(1),BFM3(2),BFM3(3),BFM3(4),BFM3(5),BFM3(6),BFM3(7) X / 0., 0., 0., 0., 1.77, 0., 0./ DATA BFP1(1),BFP1(2),BFP1(3),BFP1(4),BFP1(5),BFP1(6),BFP1(7) X / 1., 0.93, 1., 0.93, 0.93, 1., 1./ DATA BFP2(1),BFP2(2),BFP2(3),BFP2(4),BFP2(5),BFP2(6),BFP2(7) X / 0., 0.31, 0., 0.19, 0.31, 0., 0./ DATA BFP3(1),BFP3(2),BFP3(3),BFP3(4),BFP3(5),BFP3(6),BFP3(7) X / 0., 2.00, 0., 1.79, 2.00, 0., 0./ C DATA RT,RL/7.8,24./ C DATA THIRD/0.3333333/ C CURV(C1,C2,X1,X2,X3)=(C1+C2/(1.+((DE-X2)/X3)**2))* X ((DE/X1)**2)/(1.+((DE/X1)**2)) C IF(LVAR .EQ. 0) GO TO 60 IF(LVAR .LT. 5) X GO TO (10,20,30,40),LVAR C CLIMATE IF(KLIM .GT. 0. AND. KLIM .LE. 7) GO TO 51 KLIM=5 KWX=MAX0(KWX,2) 51 CV1=BV1(KLIM) CV2=BV2(KLIM) YV1=XV1(KLIM) YV2=XV2(KLIM) YV3=XV3(KLIM) CSM1=BSM1(KLIM) CSM2=BSM2(KLIM) YSM1=XSM1(KLIM) YSM2=XSM2(KLIM) YSM3=XSM3(KLIM) CSP1=BSP1(KLIM) CSP2=BSP2(KLIM) YSP1=XSP1(KLIM) YSP2=XSP2(KLIM) YSP3=XSP3(KLIM) CSD1=BSD1(KLIM) ZD=BZD1(KLIM) CFM1=BFM1(KLIM) CFM2=BFM2(KLIM) CFM3=BFM3(KLIM) CFP1=BFP1(KLIM) CFP2=BFP2(KLIM) CFP3=BFP3(KLIM) C MODE OF VARIABILITY 40 KDV=MDVAR WS=KDV .GE. 20 IF(WS) KDV=KDV-20 WL=KDV .GE. 10 IF(WL) KDV=KDV-10 IF(KDV .GE. 0 .AND. KDV .LE. 3) GO TO 41 KDV=0 KWX=MAX0(KWX,2) 41 KDV=KDV+ 1 C FREQUENCY 30 Q=ALOG(0.133*WN) GM=CFM1+CFM2/((CFM3*Q)**2+1.) GP=CFP1+CFP2/((CFP3*Q)**2+1.) C SYSTEM PARAMETERS 20 DEXA=SQRT(18E6*HE(1))+SQRT(18E6*HE(2))+(575.7E12/WN)**THIRD C DISTANCE 10 IF(DIST .GE. DEXA) GO TO 11 DE=130E3*DIST/DEXA GO TO 12 11 DE=130E3+DIST-DEXA 12 VMD=CURV( CV1 , CV2, YV1, YV2, YV3) SGTM=CURV(CSM1,CSM2,YSM1,YSM2,YSM3)*GM SGTP=CURV(CSP1,CSP2,YSP1,YSP2,YSP3)*GP SGTD=SGTP*CSD1 TGTD=(SGTP-SGTD)*ZD SGL=0. VS0=0. IF(WL) GO TO 13 Q=(1.-0.8*EXP(-AMIN1(20.,DIST/50E3)))*DH*WN SGL=10.*Q/(Q+13.) 13 IF(WS) GO TO 14 VS0=(5.+3.*EXP(-AMIN1(20.,DE/100E3)))**2 14 CONTINUE C LVAR=0 C 60 CONTINUE ZT=ZZT ZL=ZZL ZC=ZZC GO TO (600,601,602,603),KDV 600 ZT=ZC 601 ZL=ZC GO TO 603 602 ZL=ZT 603 CONTINUE IF(ABS(ZT) .GT. 3.10) GO TO 605 IF(ABS(ZL) .GT. 3.10) GO TO 605 IF(ABS(ZC) .GT. 3.10) GO TO 605 GO TO 608 605 KWX=MAX0(KWX,1) 608 CONTINUE IF(ZT .GT. 0.) GO TO 611 SGT=SGTM GO TO 618 611 IF(ZT .GT. ZD) GO TO 612 SGT=SGTP GO TO 618 612 SGT=SGTD+TGTD/ZT 618 CONTINUE VS=VS0+(SGT*ZT)**2/(RT+ZC**2)+(SGL*ZL)**2/(RL+ZC**2) GO TO (620,621,622,623),KDV 620 YR=0. SGC=SQRT(SGT**2+SGL**2+VS) GO TO 628 621 YR=SGT*ZT SGC=SQRT(SGL**2+VS) GO TO 628 622 YR=SQRT(SGT**2+SGL**2)*ZT SGC=SQRT(VS) GO TO 628 623 YR=SGT*ZT+SGL*ZL SGC=SQRT(VS) 628 CONTINUE C AVAR=AREF-VMD-YR-SGC*ZC IF(AVAR .LT. 0.) AVAR=AVAR*(29.-AVAR)/(29.-10.*AVAR) RETURN END FUNCTION QERF(Z) C THE STANDARD NORMAL COMPLEMENTARY PROBABILITY C APPROXIMATION DUE TO C. HASTINGS, JR. C MAX ERROR 7.5E-8 C DATA B1,B2,B3,B4,B5/0.319381530,-0.356563782,1.781477937, X -1.821255987,1.330274429/ DATA RP,RRT2PI/4.317008,0.398942280/ C X=Z T=ABS(X) IF(T .LT. 10.) GO TO 1 QERF=0. GO TO 2 1 T=RP/(T+RP) QERF=EXP(-0.5*X**2)*RRT2PI*((((B5*T+B4)*T+B3)*T+B2)*T+B1)*T 2 IF(X .LT. 0.) QERF=1.-QERF RETURN END FUNCTION QERFI(Q) C THE INVERSE OF QERF, GIVES THE STANDARD NORMAL DEVIATE AS A C FUNCTION OF THE COMPLEMENTARY PROBABILITY C TRUNCATED AT 0.000001 AND 0.999999 C APPROXIMATION DUE TO C. HASTINGS, JR. C MAX ERROR 4.5E-4 C DATA C0,C1,C2/2.515516698,0.802853,0.010328/ DATA D1,D2,D3/1.432788,0.189269,0.001308/ C X=0.5-Q T=AMAX1(0.5-ABS(X),0.000001) T=SQRT(-2.*ALOG(T)) QERFI=T-((C2*T+C1)*T+C0)/(((D3*T+D2)*T+D1)*T+1.) IF(X .LT. 0.) QERFI=-QERFI RETURN END SUBROUTINE QLRPS(FMHZ,ZSYS,EN0,IPOL,EPS,SGM) C PREPARES PARAMETERS C SETS-- C WN,ENS,GME,ZGND C COMMON/PROP/KWX,AREF,MDP,DIST,HG(2),WN,DH,ENS,GME,ZGND, X HE(2),DL(2),THE(2) COMPLEX ZGND C COMPLEX ZQ C DATA GMA/157E-9/ C WN=FMHZ/47.7 ENS=EN0 IF(ZSYS .NE. 0.) ENS=ENS*EXP(-ZSYS/9460.) GME=GMA*(1.-0.04665*EXP(ENS/179.3)) ZQ=CMPLX(EPS,376.62*SGM/WN) ZGND=CSQRT(ZQ-1.) IF(IPOL .NE. 0) ZGND=ZGND/ZQ RETURN END SUBROUTINE QLRA( KST, KLIMX,MDVARX) DIMENSION KST(2) C PREPARES THE LONGLEY-RICE MODEL IN THE AREA PREDICTION MODE C COMMON/PROP/KWX,AREF,MDP,DIST,HG(2),WN,DH,ENS,GME,ZGND, X HE(2),DL(2),THE(2) COMPLEX ZGND COMMON/PROPV/LVAR,SGC,MDVAR,KLIM C DO 10 J=1,2 IF(KST(J)-1) 11,12,13 11 HE(J)=HG(J) GO TO 15 12 Q=4. GO TO 14 13 Q=9. 14 IF(HG(J) .LT. 5.) Q=Q*SIN(0.3141593*HG(J)) HE(J)=HG(J)+(1.+Q)*EXP(-AMIN1(20.,2.*HG(J)/AMAX1(1E-3,DH))) 15 Q=SQRT(2.*HE(J)/GME) DL(J)=Q*EXP(-0.07*SQRT(DH/AMAX1(HE(J),5.))) THE(J)=(0.65*DH*(Q/DL(J)-1.)-2.*HE(J))/Q 10 CONTINUE C MDP=1 LVAR=MAX0(LVAR,3) IF(MDVARX .LT. 0) GO TO 21 MDVAR=MDVARX LVAR=MAX0(LVAR,4) 21 IF(KLIMX .LE. 0) GO TO 22 KLIM=KLIMX LVAR=5 22 CONTINUE RETURN END SUBROUTINE QLRPFL(PFL, KLIMX, MDVARX ) DIMENSION PFL(5) C C SETS UP AND RUNS THE LONGLEY-RICE MODEL IN THE POINT-TO-POINT C MODE USING THE TERRAIN PROFILE IN PFL. C PFL(1)=ENP, PFL(2)=XI, PFL(3)=Z(0),... C COMMON/PROP/KWX,AREF,MDP,DIST,HG(2),WN,DH,ENS,GME,ZGND, X HE(2),DL(2),THE(2) COMPLEX ZGND COMMON/PROPV/LVAR,SGC,MDVAR,KLIM C DIMENSION XL(2) C DIST=PFL(1)*PFL(2) NP=PFL(1) CALL HZNS(PFL) C FIND DELTA H DO 11 J=1,2 11 XL(J)=AMIN1(15.*HG(J),0.1*DL(J)) XL(2)=DIST-XL(2) DH=DLTHX(PFL,XL(1),XL(2)) C FIND EFFECTIVE HEIGHTS HE IF(DL(1)+DL(2) .LT. 1.5*DIST) GO TO 25 C LINE-OF-SIGHT CALL ZLSQ1(PFL,XL(1),XL(2),ZA,ZB) HE(1)=HG(1)+DIM(PFL(3),ZA) HE(2)=HG(2)+DIM(PFL(NP+3),ZB) DO 21 J=1,2 21 DL(J)=SQRT(2.*HE(J)/GME)*EXP(-0.07*SQRT(DH/AMAX1(HE(J),5.))) Q=DL(1)+DL(2) IF(Q .GT. DIST) GO TO 23 Q=(DIST/Q)**2 DO 22 J=1,2 HE(J)=HE(J)*Q 22 DL(J)=SQRT(2.*HE(J)/GME)*EXP(-0.07*SQRT(DH/AMAX1(HE(J),5.))) 23 GO TO 28 C TRANSHORIZ0N 25 CALL ZLSQ1(PFL,XL(1),0.9*DL(1),ZA,Q) CALL ZLSQ1(PFL,DIST-0.9*DL(2),XL(2),Q,ZB) HE(1)=HG(1)+DIM(PFL(3),ZA) HE(2)=HG(2)+DIM(PFL(NP+3),ZB) 28 CONTINUE C MDP=-1 LVAR=MAX0(LVAR,3) IF(MDVARX .LT. 0) GO TO 31 MDVAR=MDVARX LVAR=MAX0(LVAR,4) 31 IF(KLIMX .LE. 0) GO TO 32 KLIM=KLIMX LVAR=5 32 CONTINUE C CALL LRPROP(0.) C RETURN END FUNCTION DLTHX(PFL,X1,X2) DIMENSION PFL(5) C C COMPUTES THE TERRAIN IRREGULARITY PARAMETER DH FROM THE C PROFILE PFL BETWEEN POINTS AT X1 .LT. X2. C DIMENSION S(247) C NP=PFL(1) XA=X1/PFL(2) XB=X2/PFL(2) DLTHX=0. IF(XB-XA .LT. 2.) GO TO 80 KA=0.1*(XB-XA+8.) KA=MIN0(MAX0(4,KA),25) N=10*KA-5 KB=N-KA+1 SN=N-1 S(1)=SN S(2)=1. XB=(XB-XA)/SN K=XA+1. XA=XA-FLOAT(K) DO 10 J=1,N 11 IF(XA .LE. 0.) GO TO 12 IF(K .GE. NP) GO TO 12 XA=XA-1. K=K+1 GO TO 11 12 S(J+2)=PFL(K+3)+(PFL(K+3)-PFL(K+2))*XA 10 XA=XA+XB CALL ZLSQ1(S,0.,SN,XA,XB) XB=(XB-XA)/SN DO 15 J=1,N S(J+2)=S(J+2)-XA 15 XA=XA+XB C DLTHX=QTILE(N,S(3),KA)-QTILE(N,S(3),KB) DLTHX=DLTHX/(1.-0.8*EXP(-AMIN1(20.,(X2-X1)/50E3))) 80 RETURN END SUBROUTINE HZNS(PFL) DIMENSION PFL(5) C C TO FIND HORIZ0NS FROM ANTENNAS WITH HEIGHTS HG AT THE TWO C ENDS OF THE PROFILE PFL. C PFL(1)=ENP, PFL(2)=XI, PFL(3)=Z(D), ... C OUTPUT--DISTANCES DL, TAKE-OFF ANGLES THE. C DL=DIST IF THE PATH IS LINE OF SIGHT C COMMON/PROP/KWX,AREF,MDP,DIST,HG(2),WN,DH,ENS,GME,ZGND, X HE(2),DL(2),THE(2) COMPLEX ZGND C LOGICAL WQ C NP=PFL(1) XI=PFL(2) ZA=PFL(3)+HG(1) ZB=PFL(NP+3)+HG(2) QC=0.5*GME Q=QC*DIST THE(2)=(ZB-ZA)/DIST THE(1)=THE(2)-Q THE(2)=-THE(2)-Q DL(1)=DIST DL(2)=DIST IF(NP .LT. 2) GO TO 18 SA=0. SB=DIST WQ=.TRUE. DO 10 I=2,NP SA=SA+XI SB=SB-XI Q=PFL(I+2)-(QC*SA+THE(1))*SA-ZA IF(Q .LE. 0.) GO TO 11 THE(1)=THE(1)+Q/SA DL(1)=SA WQ=.FALSE. 11 IF(WQ) GO TO 10 Q=PFL(I+2)-(QC*SB+THE(2))*SB-ZB IF(Q .LE. 0.) GO TO 10 THE(2)=THE(2)+Q/SB DL(2)=SB 10 CONTINUE C 18 RETURN END FUNCTION QTILE(NN,A,IR) DIMENSION A(NN) C C REORDERS A SO THAT A(J),J=1 ... IR ARE ALL .GE. C ALL A(I),I=IR ... NN. IN PARTICULAR, A(IR) WILL HAVE THE SAME C VALUE IT WOULD HAVE IF A WERE COMPLETELY SORTED IN C DESCENDING ORDER. C RETURNS QTILE=A(IR) C M=1 N=NN K=MIN0(MAX0(1,IR),N) 10 CONTINUE Q=A(K) I0=M J1=N 11 CONTINUE DO 12 I=I0,N IF(A(I) .LT. Q) GO TO 13 12 CONTINUE I=N 13 J=J1 DO 14 JJ=M,J1 IF(A(J) .GT. Q) GO TO 15 14 J=J-1 J=M 15 IF(I .GE. J) GO TO 16 R=A(I) A(I)=A(J) A(J)=R I0=I+1 J1=J-1 GO TO 11 16 IF(I .GE. K) GO TO 17 A(K)=A(I) A(I)=Q M=I+1 GO TO 10 17 IF(J .LE. K) GO TO 20 A(K)=A(J) A(J)=Q N=J-1 GO TO 10 20 QTILE=Q RETURN END SUBROUTINE ZLSQ1(Z,X1,X2,Z0,ZN) DIMENSION Z(5) C C LINEAR LEAST SQUARES FIT BE'IWEEN X1, X2 TO THE FUNCTION C DESCRIBED BY Z-- C Z(1)=EN, NUMBER OF INTERVALS, Z(2) =XI, INTERVAL LENGTH, C Z(J+3), J=0,...,EN, FUNCTION VALUES. C OUTPUT-- VALUES OF THE LINE, Z0 AT 0, ZN AT XT. C XN=Z(1) XA=AINT(DIM(X1/Z(2),0.)) XB=XN-AINT(DIM(XN,X2/Z(2))) IF(XB .GT. XA) GO TO 1 XA=DIM(XA,1.) XB=XN-DIM(XN,XB+1.) 1 JA=XA JB=XB N=JB-JA XA=XB-XA X=-0.5*XA XB=XB+X A=0.5*(Z(JA+3)+Z(JB+3)) B=0.5*(Z(JA+3)-Z(JB+3))*X IF(N .LT. 2) GO TO 11 DO 10 I=2,N JA=JA+1 X=X+1. A=A+Z(JA+3) B=B+Z(JA+3)*X 10 CONTINUE 11 A=A/XA B=B*12./((XA*XA+2.)*XA) Z0=A-B*XB ZN=A+B*(XN-XB) RETURN END C PROGRAM QKAREA C *QUICK AREA* C TO ILLUSTRATE THE USE OF THE LONGLEY-RICE MODEL C IN THE AREA PREDICTION MODE C C INPUT IS IN 10-COL FIELDS, THE FIRST OF WHICH IS C A SEQUENCE OF DIGITS C IN PARTICULAR, C COL 1 IS THE *EXECUTE* COLUMN--A NON-ZERO DIGIT C WILL FORCE OUTPUT C COL 2 INDICATES THE CARD TYPE-- C C COL C 12 11,... C STOP- X0 (OR A BLANK CARD) C TITLE- X1 (NEXT CARD HAS 60-COL TITLE) C DISTANCES- X2 D0,D1,DS1,D2,DS2 C RELIABILITY- X3V QT,QL C CONFIDENCE- X4 QC1,QC2,... C ENVIRONMENT- X5C DH,N0,ZS,EPS,SGM C SYSTEM- X6NPSS FMHZ,HG1,HG2 C (ALTERNATE) X7NPSS FMHZ,HG1,HG2,DH,NS,EPS,SGM C EXECUTE- X8 C RESET- X9 C COMMON/PROP/KWX,AREF,MDP,DIST,HG(2),WN,DH,ENS,GME,ZGND, X HE(2),DL(2),THE(2) COMPLEX ZGND COMMON/PROPV/LVAR,SGC,MDVAR,KLIM C COMMON/PROPA/DLSA,DX,AEL,AK1,AK2,AED,EMD,AES,EMS,DLS(2),DLA,THA COMMON/SAVE/SAVE(50) C DIMENSION JIN(6),XIN(7) DIMENSION ITL(15) DIMENSION KST(2) DIMENSION QC(7),ZC(7),XLB(7) C LOGICAL WQIT,WCON,WTL C C THE I/O UNITS ARE DEFINED HERE DATA KIN,KOT/5,6/ C DATA GMA/157E-9/ C DATA DB/8.685890/ DATA AKM/1000./ C WQIT=.FALSE. WCON=.TRUE. GO TO 190 C 10 CONTINUE C READ INPUT SEQUENCE C 1000 FORMAT(6I1,4X,7F10.0) 1001 FORMAT(15A4) C JIN(1)=0 JIN(2)=0 READ(KIN,1000) JIN,XIN WCON=JIN(1) .EQ. 0 JQ=JIN(2) IF(JQ .NE. 0) X GO TO (110,120,130,140,150,160,170,180,190),JQ C WQIT=.TRUE. GO TO 20 110 CONTINUE READ(KIN,1001) ITL WTL=.TRUE. GO TO 20 120 CONTINUE XIN(1)=DIM(XIN(1),0.) Q=XIN(2)-XIN(1) IF(Q .GT. 0.) GO TO 121 IF(XIN(1) .EQ. 0.) GO TO 128 D0=XIN(1) DS=0. DSC=0. ND=1 NDC=0 GO TO 128 121 IF(XIN(3) .LE. 0.) XIN(3)=AMAX1(1.,AINT(Q/20.+0.5)) IF(XIN(1) .LE. 0.) XIN(1)=XIN(3) D0=XIN(1) DS=XIN(3) DSC=DS ND=DIM(XIN(2),XIN(1))/DS+1.75 NDC=0 IF(XIN(4) .LE. XIN(2)) GO TO 128 IF(XIN(5) .LE. 0.) XIN(5)=5.*XIN(3) DSC=XIN(5) JQ=(XIN(4)-XIN(2))/DSC+0.75 NDC=ND ND=ND+JQ 128 GO TO 20 130 CONTINUE MDVAR=MIN0(JIN(3),3) LVAR=MAX0(LVAR,4) QT=50. QL=50. ZT=0. ZL=0. IF(XIN(1) .LE. 0.) GO TO 131 QT=XIN(1) ZT=QERFI(QT/100.) 131 IF(XIN(2) .LE. 0.) GO TO 138 QL=XIN(2) ZL=QERFI(QL/100.) 138 GO TO 20 140 CONTINUE NC=0 DO 141 JC=1,7 IF(XIN(JC) .LE. 0.) GO TO 141 NC=NC+1 QC(NC)=XIN(JC) ZC(NC)=QERFI(QC(NC)/100.) 141 CONTINUE IF(NC .GT. 0) GO TO 148 NC=1 QC(1)=50. ZC(1)=0. 148 GO TO 20 150 CONTINUE IF(JIN(3) .LE. 0) GO TO 151 KLIM=JIN(3) LVAR=5 151 IF(XIN(1) .GE. 0.) DH=XIN(1) IF(XIN(2) .LE. 0.) GO TO 152 EN0=XIN(2) ZSYS=XIN(3) 152 IF(XIN(4) .LE. 0.) GO TO 158 EPS=XIN(4) SGM=XIN(5) 158 GO TO 20 160 CONTINUE IF(JIN(3) .EQ. 1) GO TO 161 IPOL=MIN0(JIN(4),1) KST(1)=MIN0(JIN(5),2) KST(2)=MIN0(JIN(6),2) 161 IF(XIN( 1) .GT. 0.) FMHZ=XIN( 1) IF(XIN(2) .GT. 0.) HG(1)=XIN(2) IF(XIN(3) .GT. 0.) HG(2)=XIN(3) GO TO 20 170 CONTINUE IF(JIN(3) .EQ. 1) GO TO 171 IPOL=MIN0(JIN(4),1) KST(1)=MIN0(JIN(5),2) KST(2)=MIN0(JIN(6),2) 171 IF(XIN(1) .GT. 0.) FMHZ=XIN(1) IF(XIN(2) .GT. 0.) HG(1)=XIN(2) IF(XIN(3) .GT. 0.) HG(2)=XIN(3) IF(XIN(4) .GE. 0.) DH=XIN(4) IF(XIN(5) .LE. 0.) GO TO 172 EN0=XIN(5) ZSYS=0. 172 IF(XIN(6) .LE. 0.) GO TO 178 EPS=XIN(6) SGM=XIN(7) 178 GO TO 20 180 CONTINUE WCON=.FALSE. GO TO 20 190 CONTINUE FMHZ=100. HG(1)=3. HG(2)=3. DH=90. EN0=301. ZSYS=0. EPS=15. SGM=0.005 IPOL=1 KST(1)=0 KST(2)=0 KLIM=5 MDVAR=3 LVAR=5 NC=3 QC(1)=50. QC(2)=90. QC(3)=10. QT=50. QL=50. ZC(1)=0. ZC(2)=-1.28155 ZC(3)= 1.28155 ZT=0. ZL=0. D0=10. DS=10. DSC=50. ND=22 NDC=15 WTL=.FALSE. C 20 CONTINUE IF(WCON) GO TO 30 C C EXECUTION C KWX=0 CALL QLRPS(FMHZ,ZSYS,EN0,IPOL,EPS,SGM) CALL QLRA(KST,-1,-1) C C WRITE HEADING 2001 FORMAT(1H1/1H0) 2002 FORMAT(1H ) 2010 FORMAT(3X, .62HAREA PREDICTIONS FROM THE LONGLEY-RICE MODEL, VERSION 1.2.1 ) 2011 FORMAT(3X,15A4) 2015 FORMAT(12X,9HFREQUENCY,F12.0,4H MHZ) 2016 FORMAT(6X,15HANTENNA HEIGHTS,2F8.1,2H M) 2017 FORMAT(4X,17HEFFECTIVE HEIGHTS,2F8.1, . 12H M (SITING=,I1,1H,,I1,1H)) 2018 FORMAT(5X,16HTERRAIN, DELTA H,F12.0,2H M) C c WRITE(KOT,2001) IF(WTL) GO TO 211 WRITE(KOT,2010) GO TO 212 211 WRITE(KOT,2011) ITL 212 WRITE(KOT,2002) WRITE(KOT,2002) WRITE(KOT,2015) FMHZ WRITE(KOT,2016) HG WRITE(KOT,2017) HE,KST WRITE(KOT,2018) DH WRITE(KOT,2002) C 2021 FORMAT(3X,4HPOL=,I1,6H, EPS=,F3.0,6H, SGM=,F6.3,4H S/M) 2022 FORMAT(3X,5HCLIM=,I1,5H, N0=,F4.0,5H, NS=,F4.0,4H, K=,F6.3) C Q=GMA/GME WRITE(KOT,2021) IPOL,EPS,SGM WRITE(KOT,2022) KLIM,EN0,ENS,Q WRITE(KOT,2002) C 2030 FORMAT(3X,22HSINGLE-MESSAGE SERVICE) 2031 FORMAT(3X,18HACCIDENTAL SERVICE/ . 8X,F5.1,27H PER CENT TIME AVAILABILITY) 2032 FORMAT(3X,14HMOBILE SERVICE/ . 8X,21HREQUIRED RELIABILITY-,F5.1,9H PER CENT) 2033 FORMAT(3X,17HBROADCAST SERVICE/ . 8X,21HREQUIRED RELIABILITY-,F5.1,14H PER CENT TIME/ . 29X,F5.1,19H PER CENT LOCATIONS) C IF(MDVAR .NE. 0) X GO TO (231,232,233),MDVAR C WRITE(KOT,2030) GO TO 238 231 WRITE(KOT,2031) QT GO TO 238 232 WRITE(KOT,2032) QT GO TO 238 233 WRITE(KOT,2033) QT,QL 238 WRITE(KOT,2002) C 2040 FORMAT(3X, .62HESTIMATED QUANTILES OF BASIC TRANSMISSION LOSS(DB) ) 2041 FORMAT(7X, 4HDIST, 5X , 4HFREE,4X, 15HWITH CONFIDENCE/ . 8X,2HKM,5X,6HSPACE ,7F8.1) 2045 FORMAT(2X,3F9.1,6F8.1) C C COMPUTE AND PRINT VALUES WRITE(KOT,2040) WRITE(KOT,2002) WRITE(KOT,2041) (QC(JC),JC=1,NC) WRITE(KOT,2002) DT=DS D=D0 DO 240 JD=1,ND LVAR=MAX0(1,LVAR) CALL LRPROP(D*AKM) FS=DB*ALOG(2.*WN*DIST) DO 241 JC=1,NC 241 XLB(JC)=FS+AVAR(ZT,ZL,ZC(JC)) WRITE(KOT,2045) D,FS,(XLB(JC),JC=1,NC) IF(JD .EQ. NDC) DT=DSC D=D+DT 240 CONTINUE C 2081 FORMAT(3X, .62H**WARNING- SOME PARAMETERS ARE NEARLY OUT OF RANGE. / . 3X, .62H RESULTS SHOULD BE USED WITH CAUTION. ) 2082 FORMAT(3X, .62H**NOTE- DEFAULT PARAMETERS HAVE BEEN SUBSTITUTED / . 3X, .62H FOR IMPOSSIBLE ONES. ) 2083 FORMAT(3X, .62H**WARNING- A COMBINATION OF PARAMETERS IS OUT OF RANGE. / . 3X, .62H RESULTS ARE PROBABLY INVALID. ) 2084 FORMAT(3X, .62H**WARNING- SOME PARAMETERS ARE OUT OF RANGE. / . 3X, .62H RESULTS ARE PROBABLY INVALID. ) C IF(KWX .EQ. 0) GO TO 28 C C PRINT ERROR MESSAGES WRITE(KOT,2002) GO TO (281,282,283,284),KWX 281 WRITE(KOT,2081) GO TO 28 282 WRITE(KOT,2082) GO TO 28 283 WRITE(KOT,2083) GO TO 28 284 WRITE(KOT,2084) 28 CONTINUE C 30 CONTINUE IF(.NOT. WQIT) GO TO 10 C STOP END