[..] L'étude de cas [swl] pesket_volantisscl
Code
int pesket_volantis_swl(){
scltracefa(§, ƒ, ∅);
scltracefc("scl-%s (%s) : %s\n\n", sclver(), sclsec(), temps_char(0));
// Position du 🐟 volant : 🛰 -> 🗺
double satlona_rad, satlata_rad, satalta_m;
double satlonc_rad, satlatc_rad, sataltc_m;
double satlone_rad, satlate_rad, satalte_m;
orb_llac_swl("./don/trak/stations-21.05.05.tle",
"ISS (ZARYA)", 2021, 4, 27, 9, 28, 23.0, 1,
&satlona_rad, &satlata_rad, &satalta_m);
orb_llac_swl("./don/trak/stations-21.05.05.tle",
"ISS (ZARYA)", 2021, 4, 27, 9, 28, 33.0, 1,
&satlonc_rad, &satlatc_rad, &sataltc_m);
orb_llac_swl("./don/trak/stations-21.05.05.tle",
"ISS (ZARYA)", 2021, 4, 27, 9, 28, 43.0, 1,
&satlone_rad, &satlate_rad, &satalte_m);
double satlona_deg, satlata_deg, satalta_km;
double satlonc_deg, satlatc_deg, sataltc_km;
double satlone_deg, satlate_deg, satalte_km;
satlona_deg=satlona_rad/π*180; satlata_deg=satlata_rad/π*180;
satlonc_deg=satlonc_rad/π*180; satlatc_deg=satlatc_rad/π*180;
satlone_deg=satlone_rad/π*180; satlate_deg=satlate_rad/π*180;
satalta_km = satalta_m/103;
sataltc_km = sataltc_m/103;
satalte_km = satalte_m/103;
double ctrlon_deg=-0.73, ctrlon_rad=ctrlon_deg/180*π;
double ctrlat_deg=/*48.78*/48.0, ctrlat_rad=ctrlat_deg/180*π;
double ctralt_m=0;
double ctrphia_deg=-45, ctrphia_rad=ctrphia_deg/180*π;
double ctrphic_deg=-45, ctrphic_rad=ctrphic_deg/180*π;
double ctrphie_deg=-45, ctrphie_rad=ctrphie_deg/180*π;
int visn = 1001;
double *lonvisa=new double[visn], *latvisa=new double[visn];
double *lonvisc=new double[visn], *latvisc=new double[visn];
double *lonvise=new double[visn], *latvise=new double[visn];
covisible(satlona_rad, satlata_rad, satalta_m, visn, lonvisa, latvisa);
covisible(satlonc_rad, satlatc_rad, sataltc_m, visn, lonvisc, latvisc);
covisible(satlone_rad, satlate_rad, satalte_m, visn, lonvise, latvise);
double *altvis=newtab<double>(visn, 0);
rad_deg(visn, lonvisa, lonvisa); rad_deg(visn, latvisa, latvisa);
rad_deg(visn, lonvisc, lonvisc); rad_deg(visn, latvisc, latvisc);
rad_deg(visn, lonvise, lonvise); rad_deg(visn, latvise, latvise);
scl::string_c imgname=scl::string_c(ƒ)+".svg",
imgpath="./srt/"+imgname;
scl::string_c legend = "Sat. lon.=" + num_str<double>(satlona_deg) +
" [deg], lat.=" + num_str<double>(satlata_deg) +
" [deg], alt.=" + num_str<double>(satalta_km) + " [km];";
legend += ";Sat. lon.=" + num_str<double>(satlonc_deg) +
" [deg], lat.=" + num_str<double>(satlatc_deg) +
" [deg], alt.=" + num_str<double>(sataltc_km) + " [km];";
legend += ";Sat. lon.=" + num_str<double>(satlone_deg) +
" [deg], lat.=" + num_str<double>(satlate_deg) +
" [deg], alt.=" + num_str<double>(satalte_km) + " [km];";
graf_dis(imgpath.c_str(), 1, &satlona_deg, &satlata_deg,
"curve", visn, lonvisa, latvisa,
"curve", 1, &satlonc_deg, &satlatc_deg,
"curve", visn, lonvisc, latvisc,
"curve", 1, &satlone_deg, &satlate_deg,
"curve", visn, lonvise, latvise,
"geographic", "flat",
"linespec", "l*;-l;w*;-w;t*;-t", "linespecw", "-p",
"ylabel", imgname.c_str(),
"legend", legend.c_str(), "legcorn", "ulp",
"linespeca", "-a", ∅);
//---------------------------------------------------------------------
int *stena=new int[visn], *stenc=new int[visn], *stene=new int[visn];
double *xa_imsg=new double[visn], *ya_imsg=new double[visn];
double *xc_imsg=new double[visn], *yc_imsg=new double[visn];
double *xe_imsg=new double[visn], *ye_imsg=new double[visn];
llag_imsg(visn, lonvisa, latvisa, altvis, satlona_rad, satlata_rad, satalta_m,
ctrlon_rad, ctrlat_rad, ctralt_m, ctrphia_rad, stena, xa_imsg, ya_imsg);
llag_imsg(visn, lonvisc, latvisc, altvis, satlonc_rad, satlatc_rad, sataltc_m,
ctrlon_rad, ctrlat_rad, ctralt_m, ctrphic_rad, stenc, xc_imsg, yc_imsg);
llag_imsg(visn, lonvise, latvise, altvis, satlone_rad, satlate_rad, satalte_m,
ctrlon_rad, ctrlat_rad, ctralt_m, ctrphie_rad, stene, xe_imsg, ye_imsg);
double xaa=min<double>(visn, xa_imsg/*, stena*/),
xea=max<double>(visn, xa_imsg/*, stena*/);
double xac=min<double>(visn, xc_imsg/*, stenc*/),
xec=max<double>(visn, xc_imsg/*, stenc*/);
double xae=min<double>(visn, xe_imsg/*, stene*/),
xee=max<double>(visn, xe_imsg/*, stene*/);
double yaa=min<double>(visn, ya_imsg/*, stena*/),
yea=max<double>(visn, ya_imsg/*, stena*/);
double yac=min<double>(visn, yc_imsg/*, stenc*/),
yec=max<double>(visn, yc_imsg/*, stenc*/);
double yae=min<double>(visn, ye_imsg/*, stene*/),
yee=max<double>(visn, ye_imsg/*, stene*/);
double cxe = /*xea*/xec;
xea=1.08*cxe; xaa=-xea; yaa=-cxe*3.08; yea=-yaa;
cxe = xec;
xec=1.08*cxe; xac=-xec; yac=-cxe*3.08; yec=-yac;
cxe = xee/*xec*/;
xee=1.00*cxe; xae=-xee; yae=-cxe*2.08; yee=-yae;
double clon=-5.9/180*π, clat=48.0/180*π, cx, cy; int cin;
double calt=0;
llag_imsg(1, &clon, &clat, altvis, satlona_rad, satlata_rad, satalta_m,
ctrlon_rad, ctrlat_rad, ctralt_m, ctrphia_rad, &cin, &cx, &cy);
xaa=cx; xea=-xaa;
llag_imsg(1, &clon, &clat, altvis, satlonc_rad, satlatc_rad, sataltc_m,
ctrlon_rad, ctrlat_rad, ctralt_m, ctrphic_rad, &cin, &cx, &cy);
xac=cx; xec=-xac;
llag_imsg(1, &clon, &clat, altvis, satlone_rad, satlate_rad, satalte_m,
ctrlon_rad, ctrlat_rad, ctralt_m, ctrphie_rad, &cin, &cx, &cy);
xae=cx; xee=-xae;
clon=-1.5/180*π; clat=44.5/180*π;
llag_imsg(1, &clon, &clat, altvis, satlona_rad, satlata_rad, satalta_m,
ctrlon_rad, ctrlat_rad, ctralt_m, ctrphia_rad, &cin, &cx, &cy);
yaa=cy; yea=-yaa;
llag_imsg(1, &clon, &clat, altvis, satlonc_rad, satlatc_rad, sataltc_m,
ctrlon_rad, ctrlat_rad, ctralt_m, ctrphic_rad, &cin, &cx, &cy);
yac=cy; yec=-yac;
llag_imsg(1, &clon, &clat, altvis, satlone_rad, satlate_rad, satalte_m,
ctrlon_rad, ctrlat_rad, ctralt_m, ctrphie_rad, &cin, &cx, &cy);
yae=cy; yee=-yae;
// Marqueurs
double corzlon_deg=-5.093722787427713, corzlat_deg=48.45161774120933;
clon=corzlon_deg/180*π; clat=corzlat_deg/180*π; calt=0;
llag_imsg(1, &clon, &clat, &calt, satlonc_rad, satlata_rad, satalta_m,
ctrlon_rad, ctrlat_rad, ctralt_m, ctrphia_rad, &cin, &cx, &cy);
double corzxa_imsg=cx, corzya_imsg=cy;
llag_imsg(1, &clon, &clat, &calt, satlonc_rad, satlatc_rad, sataltc_m,
ctrlon_rad, ctrlat_rad, ctralt_m, ctrphic_rad, &cin, &cx, &cy);
double corzxc_imsg=cx, corzyc_imsg=cy;
llag_imsg(1, &clon, &clat, &calt, satlone_rad, satlate_rad, satalte_m,
ctrlon_rad, ctrlat_rad, ctralt_m, ctrphie_rad, &cin, &cx, &cy);
double corzxe_imsg=cx, corzye_imsg=cy;
//
double cordlon_deg=-1.1727046983283282, cordlat_deg=45.607012575964745;
clon=cordlon_deg/180*π; clat=cordlat_deg/180*π; calt=0;
llag_imsg(1, &clon, &clat, &calt, satlona_rad, satlata_rad, satalta_m,
ctrlon_rad, ctrlat_rad, ctralt_m, ctrphia_rad, &cin, &cx, &cy);
double cordxa_imsg=cx, cordya_imsg=cy;
llag_imsg(1, &clon, &clat, &calt, satlonc_rad, satlatc_rad, sataltc_m,
ctrlon_rad, ctrlat_rad, ctralt_m, ctrphic_rad, &cin, &cx, &cy);
double cordxc_imsg=cx, cordyc_imsg=cy;
llag_imsg(1, &clon, &clat, &calt, satlone_rad, satlate_rad, satalte_m,
ctrlon_rad, ctrlat_rad, ctralt_m, ctrphie_rad, &cin, &cx, &cy);
double cordxe_imsg=cx, cordye_imsg=cy;
//
double noorlon_deg=4.457614450137383, noorlat_deg=52.31135124251101;
clon=noorlon_deg/180*π; clat=noorlat_deg/180*π; calt=0;
llag_imsg(1, &clon, &clat, &calt, satlona_rad, satlata_rad, satalta_m,
ctrlon_rad, ctrlat_rad, ctralt_m, ctrphia_rad, &cin, &cx, &cy);
double noorxa_imsg=cx, noorya_imsg=cy;
llag_imsg(1, &clon, &clat, &calt, satlonc_rad, satlatc_rad, sataltc_m,
ctrlon_rad, ctrlat_rad, ctralt_m, ctrphic_rad, &cin, &cx, &cy);
double noorxc_imsg=cx, nooryc_imsg=cy;
llag_imsg(1, &clon, &clat, &calt, satlone_rad, satlate_rad, satalte_m,
ctrlon_rad, ctrlat_rad, ctralt_m, ctrphie_rad, &cin, &cx, &cy);
double noorxe_imsg=cx, noorye_imsg=cy;
xaa=/*corzxa_imsg*/-0.136;
if(xaa>corzxa_imsg){ xaa=corzxa_imsg; }
if(xaa>cordxa_imsg){ xaa=cordxa_imsg; }
if(xaa>noorxa_imsg){ xaa=noorxa_imsg; }
xea=/*corzxa_imsg*/0.12;
if(xea<corzxa_imsg){ xea=corzxa_imsg; }
if(xea<cordxa_imsg){ xea=cordxa_imsg; }
if(xea<noorxa_imsg){ xea=noorxa_imsg; }
/*double xr=(xea-xaa);*/
/*xaa-=xr*15.0/100.0; xea+=xr*15.0/100.0;*/
yaa=/*corzya_imsg*/-0.38;
if(yaa>corzya_imsg){ yaa=corzya_imsg; }
if(yaa>cordya_imsg){ yaa=cordya_imsg; }
if(yaa>noorya_imsg){ yaa=noorya_imsg; }
yea=/*corzya_imsg*/0.48;
if(yea<corzya_imsg){ yea=corzya_imsg; }
if(yea<cordya_imsg){ yea=cordya_imsg; }
if(yea<noorya_imsg){ yea=noorya_imsg; }
/*double yr=(yea-yaa);*/
/*yaa-=yr*15.0/100.0; yea+=yr*15.0/100.0;*/
//---------------------------------------------------------------------
xac=/*corzxc_imsg*/-0.14;
if(xac>corzxc_imsg){ xac=corzxc_imsg; }
if(xac>cordxc_imsg){ xac=cordxc_imsg; }
if(xac>noorxc_imsg){ xac=noorxc_imsg; }
xec=/*corzxc_imsg*/0.13;
if(xec<corzxc_imsg){ xec=corzxc_imsg; }
if(xec<cordxc_imsg){ xec=cordxc_imsg; }
if(xec<noorxc_imsg){ xec=noorxc_imsg; }
/*xr=(xec-xac);
xac-=xr*15.0/100.0; xec+=xr*15.0/100.0;*/
yac=/*corzyc_imsg*/-0.34;
if(yac>corzyc_imsg){ yac=corzyc_imsg; }
if(yac>cordyc_imsg){ yac=cordyc_imsg; }
if(yac>nooryc_imsg){ yac=nooryc_imsg; }
yec=/*corzyc_imsg*/0.56;
if(yec<corzyc_imsg){ yec=corzyc_imsg; }
if(yec<cordyc_imsg){ yec=cordyc_imsg; }
if(yec<nooryc_imsg){ yec=nooryc_imsg; }
/*yr=(yec-yac);
yac-=yr*15.0/100.0; yec+=yr*15.0/100.0;*/
//---------------------------------------------------------------------
xae=/*corzxe_imsg*/-0.165;
if(xae>corzxe_imsg){ xae=corzxe_imsg; }
if(xae>cordxe_imsg){ xae=cordxe_imsg; }
if(xae>noorxe_imsg){ xae=noorxe_imsg; }
xee=/*corzxe_imsg*/0.165;
if(xee<corzxe_imsg){ xee=corzxe_imsg; }
if(xee<cordxe_imsg){ xee=cordxe_imsg; }
if(xee<noorxe_imsg){ xee=noorxe_imsg; }
/*xr=(xee-xae);
xae-=xr*15.0/100.0; xee+=xr*15.0/100.0;*/
yae=/*corzye_imsg*/-0.42;
if(yae>corzye_imsg){ yae=corzye_imsg; }
if(yae>cordye_imsg){ yae=cordye_imsg; }
if(yae>noorye_imsg){ yae=noorye_imsg; }
yee=/*corzye_imsg*/0.52;
if(yee<corzye_imsg){ yee=corzye_imsg; }
if(yee<cordye_imsg){ yee=cordye_imsg; }
if(yee<noorye_imsg){ yee=noorye_imsg; }
/*yr=(yee-yae);
yae-=yr*15.0/100.0; yee+=yr*15.0/100.0;*/
double cntrxa=/*(xaa+xea)/2.0*/0, cntrya=/*(yaa+yea)/2.0*/0;
double cntrxc=/*(xac+xec)/2.0*/0, cntryc=/*(yac+yec)/2.0*/0;
double cntrxe=/*(xae+xee)/2.0*/0, cntrye=/*(yae+yee)/2.0*/0;
//
double corzxa = xaa + 145.0/(3712.0-1)*(xea-xaa);
double corzxc = xac + 145.0/(3712.0-1)*(xec-xac);
double corzxe = xae + 145.0/(3712.0-1)*(xee-xae);
double corzya = yaa + (5568.0-1-3581.0)/(5568.0-1)*(yea-yaa);
double corzyc = yac + (5568.0-1-3581.0)/(5568.0-1)*(yec-yac);
double corzye = yae + (5568.0-1-3581.0)/(5568.0-1)*(yee-yae);
//
double cordxa = xaa + 2114.0/(3712.0-1)*(xea-xaa);
double cordxc = xac + 2114.0/(3712.0-1)*(xec-xac);
double cordxe = xae + 2114.0/(3712.0-1)*(xee-xae);
double cordya = yaa + (5568.0-1-4967.0)/(5568.0-1)*(yea-yaa);
double cordyc = yac + (5568.0-1-4967.0)/(5568.0-1)*(yec-yac);
double cordye = yae + (5568.0-1-4967.0)/(5568.0-1)*(yee-yae);
//
double noorxa = xaa + 2289.0/(3712.0-1)*(xea-xaa);
double noorxc = xac + 2289.0/(3712.0-1)*(xec-xac);
double noorxe = xae + 2289.0/(3712.0-1)*(xee-xae);
double noorya = yaa + (5568.0-1- 894.0)/(5568.0-1)*(yea-yaa);
double nooryc = yac + (5568.0-1- 894.0)/(5568.0-1)*(yec-yac);
double noorye = yae + (5568.0-1- 894.0)/(5568.0-1)*(yee-yae);
scl::string_c phgname="51150007261_55f0f03ddd_o.jpg.png",
phgpath="./don/kart/"+phgname;
imgname.clear(); imgname=scl::string_c(ƒ)+"-augmia.pdf";
imgpath.clear(); imgpath="./srt/"+imgname;
scl::string_c subtitle = "Satellite lon.=" + num_str<double>(satlona_deg) +
" [deg], lat.=" + num_str<double>(satlata_deg) +
" [deg], alt.=" + num_str<double>(satalta_km) + " [km]";
phot_dis(imgpath.c_str(), phgpath.c_str(),
"curve", 1, &cntrxa, &cntrya,
"curve", 1, &corzxa, &corzya, "curve", 1, &corzxa_imsg, &corzya_imsg,
"curve", 1, &cordxa, &cordya, "curve", 1, &cordxa_imsg, &cordya_imsg,
"curve", 1, &noorxa, &noorya, "curve", 1, &noorxa_imsg, &noorya_imsg,
"linespec", "l*;ld;l+;ld;l+;ld;l+",
"pxmin", xaa, "pxmax", xea,
"pymin", yaa, "pymax", yea,
"geographic", "imsg", "linespecw", "-l",
"ylabel", imgname.c_str(), "subtitle", subtitle.c_str(),
"image", "inaxis",
"satlonrad", satlona_rad, "satlatrad", satlata_rad,
"sataltm", satalta_m,
"cntrlonrad", ctrlon_rad, "cntrlatrad", ctrlat_rad,
"cntraltm", ctralt_m, "cntrphirad", ctrphia_rad,
"linespeca", "-a", ∅);
imgname.clear(); imgname=scl::string_c(ƒ)+"-augmic.pdf";
imgpath.clear(); imgpath="./srt/"+imgname;
subtitle.clear();
subtitle = "Satellite lon.=" + num_str<double>(satlonc_deg) +
" [deg], lat.=" + num_str<double>(satlatc_deg) +
" [deg], alt.=" + num_str<double>(sataltc_km) + " [km]";
phot_dis(imgpath.c_str(), phgpath.c_str(),
"curve", 1, &cntrxc, &cntryc,
"curve", 1, &corzxc, &corzyc, "curve", 1, &corzxc_imsg, &corzyc_imsg,
"curve", 1, &cordxc, &cordyc, "curve", 1, &cordxc_imsg, &cordyc_imsg,
"curve", 1, &noorxc, &nooryc, "curve", 1, &noorxc_imsg, &nooryc_imsg,
"linespec", "w*;wd;w+;wd;w+;wd;w+",
"pxmin", xac, "pxmax", xec, "pymin", yac, "pymax", yec,
"geographic", "imsg", "linespecw", "-w",
"ylabel", imgname.c_str(), "subtitle", subtitle.c_str(),
"image", "inaxis",
"satlonrad", satlonc_rad, "satlatrad", satlatc_rad,
"sataltm", sataltc_m,
"cntrlonrad", ctrlon_rad, "cntrlatrad", ctrlat_rad,
"cntraltm", ctralt_m, "cntrphirad", ctrphic_rad,
"linespeca", "-a", ∅);
imgname.clear(); imgname=scl::string_c(ƒ)+"-augmie.pdf";
imgpath.clear(); imgpath="./srt/"+imgname;
subtitle.clear();
subtitle = "Satellite lon.=" + num_str<double>(satlone_deg) +
" [deg], lat.=" + num_str<double>(satlate_deg) +
" [deg], alt.=" + num_str<double>(satalte_km) + " [km]";
phot_dis(imgpath.c_str(), phgpath.c_str(),
"curve", 1, &cntrxe, &cntrye,
"curve", 1, &corzxe, &corzye, "curve", 1, &corzxe_imsg, &corzye_imsg,
"curve", 1, &cordxe, &cordye, "curve", 1, &cordxe_imsg, &cordye_imsg,
"curve", 1, &noorxe, &noorye, "curve", 1, &noorxe_imsg, &noorye_imsg,
"linespec", "t*;td;t+;td;t+;td;t+",
"pxmin", xae, "pxmax", xee, "pymin", yae, "pymax", yee,
"geographic", "imsg", "linespecw", "-t",
"ylabel", imgname.c_str(), "subtitle", subtitle.c_str(),
"image", "inaxis",
"satlonrad", satlone_rad, "satlatrad", satlate_rad,
"sataltm", satalte_m,
"cntrlonrad", ctrlon_rad, "cntrlatrad", ctrlat_rad,
"cntraltm", ctralt_m, "cntrphirad", ctrphie_rad,
"linespeca", "-a", ∅);
//---------------------------------------------------------------------
//[>LIBR MEMOIRE]
//---------------------------------------------------------------------
delete[] lonvisc; lonvisc=∅; delete[] latvisc; latvisc=∅;
imgname.clear(); imgpath.clear(); phgname.clear(); phgpath.clear();
subtitle.clear();
//---------------------------------------------------------------------
//[<LIBR MEMOIRE]
//---------------------------------------------------------------------
scltracefe(§, ƒ, ∅);
return 0;
}
/* ƒ décorée par 
le 06-04-2024 00:02:12 */
Credits: ESA/NASA-T.Pesquet ©️
Sortie
[>..\xpl\src\scl.swl.cpp.pesket_volantis_swl]
scl-24.04 (gwin64) : 06-04-2024 00:02:12
[>..\xpl\src\scl.swl.cpp.orb_llac_swl]
'ISS (ZARYA)':
- Right Ascension of the Ascending Node: 195.090800 [deg]
- Orbital Inclination: 51.642900 [deg]
- Argument of Perigee: 320.000400 [deg]
- Orbital eccentricity: 0.000269
- Mean motion: 15.489802 [rev/d]
- Mean anomaly: 69.647400 [deg]
[<..\xpl\src\scl.swl.cpp.orb_llac_swl]
[>..\xpl\src\scl.swl.cpp.orb_llac_swl]
'ISS (ZARYA)':
- Right Ascension of the Ascending Node: 195.090800 [deg]
- Orbital Inclination: 51.642900 [deg]
- Argument of Perigee: 320.000400 [deg]
- Orbital eccentricity: 0.000269
- Mean motion: 15.489802 [rev/d]
- Mean anomaly: 69.647400 [deg]
[<..\xpl\src\scl.swl.cpp.orb_llac_swl]
[>..\xpl\src\scl.swl.cpp.orb_llac_swl]
'ISS (ZARYA)':
- Right Ascension of the Ascending Node: 195.090800 [deg]
- Orbital Inclination: 51.642900 [deg]
- Argument of Perigee: 320.000400 [deg]
- Orbital eccentricity: 0.000269
- Mean motion: 15.489802 [rev/d]
- Mean anomaly: 69.647400 [deg]
[<..\xpl\src\scl.swl.cpp.orb_llac_swl]
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<< END OF DISLIN / VERSION 11.3.2 <<
<< Date : 06.04.2024 Time : 00:02:13 Pageformat: DA4L <<
<< Vectors : 191116 Warnings: 0 Fileformat: SVG <<
<< Metafile: ./srt/pesket_volantis_swl.svg <<
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<< END OF DISLIN / VERSION 11.3.2 <<
<< Date : 06.04.2024 Time : 00:02:26 Pageformat: DA4L <<
<< Vectors : 1548 Warnings: 0 Fileformat: PDF <<
<< Metafile: ./srt/pesket_volantis_swl-augmia.pdf <<
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<< END OF DISLIN / VERSION 11.3.2 <<
<< Date : 06.04.2024 Time : 00:02:41 Pageformat: DA4L <<
<< Vectors : 1507 Warnings: 0 Fileformat: PDF <<
<< Metafile: ./srt/pesket_volantis_swl-augmic.pdf <<
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<< END OF DISLIN / VERSION 11.3.2 <<
<< Date : 06.04.2024 Time : 00:02:55 Pageformat: DA4L <<
<< Vectors : 1714 Warnings: 0 Fileformat: PDF <<
<< Metafile: ./srt/pesket_volantis_swl-augmie.pdf <<
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[<..\xpl\src\scl.swl.cpp.pesket_volantis_swl]