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YASim CLI tool: add more CG outputs

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remove non-significant digits from inertia printf()
This commit is contained in:
Henning Stahlke 2017-12-01 12:54:43 +01:00
parent 78f7950fa6
commit abb451256d
1 changed files with 10 additions and 8 deletions
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18
src/FDM/YASim/yasim-test.cpp
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@ -260,16 +260,18 @@ int main(int argc, char** argv)
printf("Approach Elevator: %.3f\n\n", a->getApproachElevator());
printf(" CG: x:%.3f, y:%.3f, z:%.3f\n", cg[0], cg[1], cg[2]);
if (wing) {
printf(" Wing MAC (*1): x:%.2f, y:%.2f, length:%.1f \n", MACx, MACy, MAC);
printf(" CG-x rel. MAC: %.3f\n", a->getCGMAC());
printf(" CG-x desired: %.3f < %.3f < %.3f \n", a->getCGSoftLimitXMin(), cg[0], a->getCGSoftLimitXMax());
printf(" Wing MAC: (x:%.2f, y:%.2f), length:%.1f \n", MACx, MACy, MAC);
printf(" hard limit CG-x: %.3f \n", a->getCGHardLimitXMax());
printf(" soft limit CG-x: %.3f \n", a->getCGSoftLimitXMax());
printf(" CG-x: %.3f \n", cg[0]);
printf(" CG-x rel. MAC: %3.0f%%\n", a->getCGMAC()*100);
printf(" soft limit CG-x: %.3f \n", a->getCGSoftLimitXMin());
printf(" hard limit CG-x: %.3f \n", a->getCGHardLimitXMin());
}
printf("\nInertia tensor [kg*m^2], origo at CG:\n\n");
printf(" %7.3f, %7.3f, %7.3f\n", SI_inertia[0], SI_inertia[1], SI_inertia[2]);
printf(" %7.3f, %7.3f, %7.3f\n", SI_inertia[3], SI_inertia[4], SI_inertia[5]);
printf(" %7.3f, %7.3f, %7.3f\n", SI_inertia[6], SI_inertia[7], SI_inertia[8]);
printf("\n(*1) MAC calculation works on <wing> only! Numbers will be wrong for segmented wings, e.g. <wing>+<mstab>.\n");
printf(" %7.0f, %7.0f, %7.0f\n", SI_inertia[0], SI_inertia[1], SI_inertia[2]);
printf(" %7.0f, %7.0f, %7.0f\n", SI_inertia[3], SI_inertia[4], SI_inertia[5]);
printf(" %7.0f, %7.0f, %7.0f\n", SI_inertia[6], SI_inertia[7], SI_inertia[8]);
}
delete fdm;
return 0;