142 |
TY = TAN(ASIN(AL_P(3))) * SIN(AL_P(4)) |
TY = TAN(ASIN(AL_P(3))) * SIN(AL_P(4)) |
143 |
DO I = 1, NPLA |
DO I = 1, NPLA |
144 |
NN = 0 |
NN = 0 |
145 |
C????? IF (M.EQ.2) NN = 1 |
IF (M.EQ.2) NN = 1 |
146 |
IF (MOD(I,2).EQ.NN) THEN |
IF (MOD(I,2).EQ.NN) THEN |
147 |
SHIFT = +0.5 |
SHIFT = +0.5 |
148 |
ELSE |
ELSE |
268 |
C |
C |
269 |
DO I = 1,NPLA |
DO I = 1,NPLA |
270 |
NN = 0 |
NN = 0 |
271 |
C????? IF (M.EQ.2) NN = 1 |
IF (M.EQ.2) NN = 1 |
272 |
IF (MOD(I,2).EQ.NN) THEN |
IF (MOD(I,2).EQ.NN) THEN |
273 |
SHIFT = +0.5 |
SHIFT = +0.5 |
274 |
ELSE |
ELSE |
372 |
RNSS = 0. |
RNSS = 0. |
373 |
QTOTT = 0. |
QTOTT = 0. |
374 |
C |
C |
375 |
PPLANEMAX = 1.01*(LOG(ABS(RIG)/0.0081)-1.) |
PPLANEMAX = 1.01*(LOG(ABS(RIG)/0.0081)-1.) / 0.74 |
376 |
C |
C |
377 |
IPLANE = INT(ANINT(PPLANEMAX)) + 5 |
IPLANE = INT(ANINT(PPLANEMAX)) + 5 |
378 |
C |
C |
401 |
C |
C |
402 |
DO J = 1,IPLANE |
DO J = 1,IPLANE |
403 |
NNX = IBAR(1,J) |
NNX = IBAR(1,J) |
404 |
|
RNSS = 0. ! BACO!! |
405 |
|
QTOTT = 0. ! BACO!! |
406 |
IF (NNX.NE.-1) THEN |
IF (NNX.NE.-1) THEN |
407 |
IF (NNX.LT.9) NNX = 9 |
IF (NNX.LT.9) NNX = 9 |
408 |
IF (NNX.GT.88) NNX = 88 |
IF (NNX.GT.88) NNX = 88 |