#include <stdio.h>
+#include <cstring>
+#include <cstdlib>
+
#include <simgear/props/props.hxx>
#include <simgear/xml/easyxml.hxx>
bool fgSetFloat (const char * name, float val) { return false; }
bool fgSetBool(char const * name, bool val) { return false; }
bool fgGetBool(char const * name, bool def) { return false; }
+bool fgSetString(char const * name, char const * str) { return false; }
SGPropertyNode* fgGetNode (const char * path, bool create) { return 0; }
SGPropertyNode* fgGetNode (const char * path, int i, bool create) { return 0; }
float fgGetFloat (const char * name, float defaultValue) { return 0; }
for(int deg=-179; deg<=179; deg++) {
float aoa = deg * DEG2RAD;
- Airplane::setupState(aoa, kts * KTS2MPS, &s);
+ Airplane::setupState(aoa, kts * KTS2MPS, 0 ,&s);
m->getBody()->reset();
m->initIteration();
m->calcForces(&s);
if(!a->getFailureMsg() && argc > 2 && strcmp(argv[2], "-g") == 0) {
float alt = 5000, kts = 100;
for(int i=3; i<argc; i++) {
- if (strcmp(argv[i], "-a") == 0) alt = atof(argv[++i]);
- else if(strcmp(argv[i], "-s") == 0) kts = atof(argv[++i]);
+ if (std::strcmp(argv[i], "-a") == 0) alt = std::atof(argv[++i]);
+ else if(std::strcmp(argv[i], "-s") == 0) kts = std::atof(argv[++i]);
else return usage();
}
yasim_graph(a, alt, kts);
float drag = 1000 * a->getDragCoefficient();
float cg[3];
a->getModel()->getBody()->getCG(cg);
+ a->getModel()->getBody()->recalc();
+
+ float SI_inertia[9];
+ a->getModel()->getBody()->getInertiaMatrix(SI_inertia);
printf("Solution results:");
printf(" Iterations: %d\n", a->getSolutionIterations());
printf(" Cruise AoA: %f\n", aoa);
printf(" Tail Incidence: %f\n", tail);
printf("Approach Elevator: %f\n", a->getApproachElevator());
- printf(" CG: %.3f, %.3f, %.3f\n", cg[0], cg[1], cg[2]);
+ printf(" CG: x:%.3f, y:%.3f, z:%.3f\n\n", cg[0], cg[1], cg[2]);
+ printf(" Inertia tensor : %.3f, %.3f, %.3f\n", SI_inertia[0], SI_inertia[1], SI_inertia[2]);
+ printf(" [kg*m^2] %.3f, %.3f, %.3f\n", SI_inertia[3], SI_inertia[4], SI_inertia[5]);
+ printf(" Origo at CG %.3f, %.3f, %.3f\n", SI_inertia[6], SI_inertia[7], SI_inertia[8]);
}
delete fdm;
return 0;