From abb451256dc4bfd8ce1552c03ef06c7d42863c08 Mon Sep 17 00:00:00 2001
From: Henning Stahlke <github@henningstahlke.de>
Date: Fri, 1 Dec 2017 12:54:43 +0100
Subject: [PATCH] YASim CLI tool: add more CG outputs remove non-significant
digits from inertia printf()
---
src/FDM/YASim/yasim-test.cpp | 18 ++++++++++--------
1 file changed, 10 insertions(+), 8 deletions(-)
diff --git a/src/FDM/YASim/yasim-test.cpp b/src/FDM/YASim/yasim-test.cpp
index d4f9f1518..685164756 100644
--- a/src/FDM/YASim/yasim-test.cpp
+++ b/src/FDM/YASim/yasim-test.cpp
@@ -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;