1 | MODULE solarlong_mod |
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2 | |
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3 | IMPLICIT NONE |
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4 | |
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5 | CONTAINS |
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6 | |
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7 | SUBROUTINE solarlong(pday,psollong) |
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8 | use planete_h, only: lsperi, peri_day, year_day, e_elips |
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9 | use comcstfi_h, only: pi |
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10 | IMPLICIT NONE |
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11 | |
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12 | c======================================================================= |
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13 | c Compute solar longitude psollong (in radians) for a given Mars date |
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14 | c pday (where pday==0 at northern Spring Equinox and pday in sols |
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15 | c and fractions thereof) |
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16 | c======================================================================= |
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17 | |
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18 | c arguments: |
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19 | c ---------- |
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20 | |
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21 | REAL,INTENT(IN) :: pday |
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22 | REAL,INTENT(OUT) :: psollong |
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23 | |
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24 | c Local variables: |
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25 | c ---------------- |
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26 | |
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27 | REAL :: xref ! mean anomaly |
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28 | REAL :: zx0 ! eccentric anomaly |
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29 | REAL :: zteta ! true anomaly |
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30 | REAL :: zanom,zdx,zz |
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31 | INTEGER :: iter |
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32 | |
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33 | |
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34 | c compute mean anomaly |
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35 | |
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36 | zz=(pday-peri_day)/year_day |
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37 | pi=2.*asin(1.) |
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38 | zanom=2.*pi*(zz-nint(zz)) |
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39 | xref=abs(zanom) |
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40 | |
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41 | c solve equation zx0 - e * sin (zx0) = xref |
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42 | c using Newton method |
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43 | |
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44 | zx0=xref+e_elips*sin(xref) |
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45 | DO iter=1,10 ! 10 is overkill, typically converges in 1-3 iterations |
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46 | zdx=-(zx0-e_elips*sin(zx0)-xref)/(1.-e_elips*cos(zx0)) |
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47 | if(abs(zdx).le.(1.e-7)) exit |
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48 | zx0=zx0+zdx |
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49 | ENDDO |
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50 | |
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51 | zx0=zx0+zdx |
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52 | if(zanom.lt.0.) zx0=-zx0 |
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53 | |
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54 | c compute true anomaly zteta, now that eccentric anomaly zx0 is known |
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55 | |
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56 | zteta=2.*atan(sqrt((1.+e_elips)/(1.-e_elips))*tan(zx0/2.)) |
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57 | |
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58 | c compute solar longitude from zteta |
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59 | psollong=zteta+lsperi |
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60 | |
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61 | c handle limit cases where psollong lands outside [0:2*pi] |
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62 | IF(psollong.LT.0.) psollong=psollong+2.*pi |
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63 | IF(psollong.GT.2.*pi) psollong=psollong-2.*pi |
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64 | |
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65 | END SUBROUTINE solarlong |
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66 | |
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67 | END MODULE solarlong_mod |
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