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ctxcal now uses cam #4304

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merged 4 commits into from
Feb 24, 2021
Merged

ctxcal now uses cam #4304

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f17a899
ctxcal now uses cam
Feb 22, 2021
245e512
added checkerror calls
Feb 22, 2021
302bc5b
removed some check status
Feb 23, 2021
835a03b
import NaifStatus
Feb 23, 2021
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40 changes: 25 additions & 15 deletions isis/src/mro/apps/ctxcal/main.cpp
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Original file line number Diff line number Diff line change
Expand Up @@ -15,6 +15,7 @@ find files of those names at the top level of this repository. **/
#include "LineManager.h"
#include "Brick.h"
#include "Table.h"
#include "Camera.h"

using namespace std;
using namespace Isis;
Expand Down Expand Up @@ -139,21 +140,30 @@ void IsisMain() {
// iof = conversion factor from counts/ms to i/f
bool convertIOF = ui.GetBoolean("IOF");
if(convertIOF) {
// Get the distance between Mars and the Sun at the given time in
// Astronomical Units (AU)
QString bspKernel = p.MissionData("base", "/kernels/spk/de???.bsp", true);
furnsh_c(bspKernel.toLatin1().data());
QString satKernel = p.MissionData("base", "/kernels/spk/mar???.bsp", true);
furnsh_c(satKernel.toLatin1().data());
QString pckKernel = p.MissionData("base", "/kernels/pck/pck?????.tpc", true);
furnsh_c(pckKernel.toLatin1().data());
double sunpos[6], lt;
spkezr_c("sun", etStart, "iau_mars", "LT+S", "mars", sunpos, &lt);
double dist1 = vnorm_c(sunpos);
unload_c(bspKernel.toLatin1().data());
unload_c(satKernel.toLatin1().data());
unload_c(pckKernel.toLatin1().data());

double dist1 = 1;
try {
Camera *cam;
cam = icube->camera();
cam->setTime(startTime);
dist1 = cam->sunToBodyDist();
}
catch(IException &e) {
// Get the distance between Mars and the Sun at the given time in
// Astronomical Units (AU)
QString bspKernel = p.MissionData("base", "/kernels/spk/de???.bsp", true);
furnsh_c(bspKernel.toLatin1().data());
QString satKernel = p.MissionData("base", "/kernels/spk/mar???.bsp", true);
furnsh_c(satKernel.toLatin1().data());
QString pckKernel = p.MissionData("base", "/kernels/pck/pck?????.tpc", true);
furnsh_c(pckKernel.toLatin1().data());
double sunpos[6], lt;
spkezr_c("sun", etStart, "iau_mars", "LT+S", "mars", sunpos, &lt);
dist1 = vnorm_c(sunpos);
unload_c(bspKernel.toLatin1().data());
unload_c(satKernel.toLatin1().data());
unload_c(pckKernel.toLatin1().data());
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}

double dist = 2.07E8;
double w0 = 3660.5;
double w1 = w0 * ((dist * dist) / (dist1 * dist1));
Expand Down