1 | * |
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2 | * ... THIS FUNCTION RETURNS THE MIE TRANSITION FACTOR ... |
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3 | * ... IN THE ATMOSPHERE BETWEEN THE POINTS WITH ... |
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4 | * ... RADIUS_VECTORS R(3) AND ISS |
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5 | * ... DATE: 09.06.2002 |
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6 | * ... AUTHOR: D.V. NAUMOV |
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7 | * |
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8 | REAL FUNCTION MIE_R_ISS(R) |
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9 | IMPLICIT NONE |
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10 | #include "detector.inc" |
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11 | #include "event.inc" |
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12 | * ... EXTERNAL CALLS ... |
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13 | REAL HXY |
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14 | * ... INPUT VARIABLES ... |
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15 | REAL R(3) |
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16 | * ... LOCAL VARIABLES ... |
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17 | INTEGER i_aux_hbk, ID |
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18 | REAL PI,HALF_PI,MIE_R |
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19 | REAL RTOISS(3), H_R,THETA_R, DEPTH_R, SCALAR_R |
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20 | REAL SCALAR_ISS_RTOISS,SCALAR_ISS,SCALAR_RTOISS,cos_R_ISS |
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21 | SAVE i_aux_hbk |
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22 | DATA i_aux_hbk/0/ |
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23 | LOGICAL HEXIST |
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24 | * |
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25 | PI = ACOS(-1.) |
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26 | HALF_PI = PI/2 |
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27 | ID = 10000 |
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28 | * |
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29 | CALL VECTORLIB(3,'-',ISS,R,RTOISS) |
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30 | CALL VECTORDOT(3,ISS,RTOISS,SCALAR_ISS_RTOISS) |
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31 | CALL VECTORDOT(3,ISS,ISS,SCALAR_ISS) |
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32 | CALL VECTORDOT(3,RTOISS,RTOISS,SCALAR_RTOISS) |
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33 | CALL VECTORDOT(3,R,R,SCALAR_R) |
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34 | IF(SCALAR_ISS*SCALAR_RTOISS.NE.0.) THEN |
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35 | cos_R_ISS = SCALAR_ISS_RTOISS/SQRT(SCALAR_ISS*SCALAR_RTOISS) |
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36 | ELSE |
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37 | cos_R_ISS = 0. |
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38 | ENDIF |
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39 | THETA_R = ACOS(cos_R_ISS) |
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40 | H_R = SQRT(SCALAR_R) - R_EARTH |
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41 | * ... COMPUTE MIE FACTORS BETWEEN R AND INFINITY ... |
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42 | IF(THETA_R.LE.HALF_PI) THEN |
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43 | MIE_R = HXY(ID,THETA_R,H_R) |
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44 | ELSE |
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45 | MIE_R = 0. |
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46 | ENDIF |
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47 | * ... COMPUTE MIE FACTOR BETWEEN R1 AND R2 ... |
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48 | MIE_R_ISS = EXP(-MIE_R) |
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49 | |
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50 | 1000 CONTINUE |
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51 | END |
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