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motion_3d_cartesian_rail.c
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motion_3d_cartesian_rail.c
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#include "Dynamics/dynamics_3d_cartesian_rail.h"
//#include "Dynamics/winds.h"
#include <time.h>
#include <string.h>
#include <stdbool.h>
#define _theta0 PI/2.
#define _phi0 0.
#define _dtheta0 -0.5
#define _dphi0 0.
#define dim 3
#define mu 0.//0.261799//=15 //0.0872665=5 RADIANS!!!
// ============== FILE INPUT: ATTACK ANGLE AND WIND X, Y, Z, THETA0 AND PHI0 ============
int main(int argc, char *argv[]){
// ========================= READING INPUT VARIABLES ==========================
if (argc <= 4){
printf("Missing inputs!!! Need ATTACK ANGLE INDEX, WIND X, WIND Y, WIND Z, THETA0 AND PHI0\n");
return 0;
}
int alpha_index = atoi( *(argv + 1) );
double W[3];
W[0] = atof( *(argv + 2) );
W[1] = atof( *(argv + 3) );
W[2] = atof( *(argv + 4) );
double theta = _theta0;
double phi = _phi0;
double dtheta = _dtheta0;
double dphi = _dphi0;
double sp=0, pv=0;
if (alpha_index >= n_alphas){
printf("Alpha index too big!!!\n");
return 0;
}
// ========================= OUTPUT FILES ==========================
FILE *trajectory, *debug;
trajectory = fopen("out.txt", "w+");
debug = fopen("debug3d.csv", "w+");
//fprintf(trajectory, "t,x_kite,y_kite,z_kite,x_block,y_block,z_block,theta,vtheta,windx,windy,wind_z,v_blockx,v_blocky,Tension\n");
fprintf(debug, "i,Alpha,mu,theta,Windx,Windy,Windz,Vkx,Vky,Vkz,Lift,Liftx,Lifty,Liftz,Drag,Tension,F_attrito,sector,uno,due,tre,1-sp,angle,prod_vect,t2[0],t2[1],t2[2]\n");
// ============================ VARIABLES DEFINITION ============================
// kite motion vectors from fixed origin (x, z)
double *rk = (double*) malloc(dim * sizeof(double));
double *vk = (double*) malloc(dim * sizeof(double));
double *ak = (double*) malloc(dim * sizeof(double));
// block motion vectors from fixed origin (x, z)
double *r_block = (double*) malloc(dim * sizeof(double));
double *v_block = (double*) malloc(dim * sizeof(double));
double *a_block = (double*) malloc(dim * sizeof(double));
// block motion vectors from fixed origin (x, z)
double *r_diff = (double*) malloc(dim * sizeof(double));
double *v_diff = (double*) malloc(dim * sizeof(double));
double *a_diff = (double*) malloc(dim * sizeof(double));
double r_diff_modulo;
double v_diff_modulo;
double lift=0, drag=0;
double T = 0;
double F_attr;
double F_vinc;
double theta_star;
int stability = 0;
int decollato = 0;
int sector = 0;
double l0, l1, l2;
double d0, d1, d2;
variables_initialization(rk, vk, ak, theta, phi, dtheta, dphi, r_block, v_block, a_block, r_diff, v_diff, a_diff);
//streamfunction3d(rk, W);
int t = 0;
// ============================ KITE FLYING LOOP, STOPS WHEN FALL OCCURS ============================
for (int i=0; i<STEPS; i++){
integration_trajectory(rk, vk, ak, r_block, v_block, a_block, r_diff, v_diff, a_diff, \
&theta, &phi, alpha_index, mu, W, &lift, &drag, &T, &F_attr, i, §or, \
&l0, &l1, &l2, &d0, &d1, &d2);//, &uno, &due, &tre, &sp, &pv, t22);
//printf("\ni=%d, L=%f, D=%f, T=%f, F_attr=%f, sector=%d\n", i, lift, drag, T, fabs(F_attr), sector);
//printf("Lx=%f, Ly=%f, Lz=%f\n", l0, l1, l2);
r_diff_modulo = sqrt(r_diff[0]*r_diff[0] + r_diff[1]*r_diff[1] + r_diff[2]*r_diff[2]);
F_vinc = m_block*g - T*sin(theta);
// moving the kite to put it again at distance R with the block
rk[0] = r_block[0] + (rk[0] - r_block[0])/fabs(r_diff_modulo)*R;
rk[1] = r_block[1] + (rk[1] - r_block[1])/fabs(r_diff_modulo)*R;
rk[2] = r_block[2] + (rk[2] - r_block[2])/fabs(r_diff_modulo)*R;
//streamfunction3d(rk, W);
if (i%1 == 0){
fprintf(debug, "%d,%.2f,%.2f,%.2f,%.2f,%.2f,%.2f,%.2f,%f,%f,%f,%f,%f,%f,%f,%f,%f,%d\n", \
i, alphas[alpha_index], mu, theta, W[0], W[1], W[2], vk[0], vk[1], vk[2], lift, l0, l1, l2, drag, T, \
fabs(F_attr), sector);
}
if (i%PRINTSTEP == 0 || rk[2] <= 0.){
//fprintf(trajectory, "%d,%f,%f,%f,%f,%f,%f,%f,%f,%f,%f,%f,%f,%f,%f\n", \
t, rk[0], rk[1], rk[2], r_block[0], r_block[1],r_block[2], theta, dtheta, \
W[0], W[1], W[2], v_block[0], v_block[1],T);
if (rk[2] <=0. ){
//printf("Kite Fall, steps %d, z<0, break\n", i);
break;
}
}
t += 1;
if (F_vinc < 0) {
decollato = 1;
}
}
v_diff_modulo = sqrt(v_diff[0]*v_diff[0] + v_diff[1]*v_diff[1] + v_diff[2]*v_diff[2]);
dtheta = -1/(sqrt(1-(r_diff[2]/r_diff_modulo)*(r_diff[2]/r_diff_modulo)))*(v_diff[2]*r_diff_modulo-r_diff[2]*v_diff_modulo)/(r_diff_modulo*r_diff_modulo);
dphi = 1/(1+(r_diff[1]/r_diff[0])*(r_diff[1]/r_diff[0]))*(v_diff[1]*r_diff[0] - r_diff[0]*v_diff[1])/(r_diff[0]*r_diff[0]);
if (rk[2] <= 0){
rk[2] = 0;
v_block[0] = 0;
v_block[1] = 0;
vk[0] = 0;
vk[1] = 0;
vk[2] = 0;
theta = PI/2;
dtheta = 0;
}
//printf("\niter, tot time, m_block, alpha, mu, theta0, theta_fin, v_block_fin_x, v_block_fin_y, Wind_x, Wind_y, Wind_z");
//printf(" Vkitex, Vkitey, Vkitez, vrelkite_x, vrelkite_y, vrelkite_z, F_vinc, Tension, Lift, l0, l1, l2, Drag, d0, d1, d2\n");
printf("%d, %.2f, %.2f, %.2f, %.2f, %.2f, %.2f, %.2f, %.2f, %.2f, %.2f, %.2f, %.2f, %.2f, %.2f, %.2f, %.2f, %.2f, %.2f, %.2f, %.2f, %.2f, %.2f, %.2f, %.2f, %.2f, %.2f, %.2f, %.2f\n", \
t, t*h, m_block, alphas[alpha_index], mu, _theta0, theta, dtheta, v_block[0], v_block[1], W[0], W[1], W[2], \
vk[0], vk[1], vk[2], vk[0] - W[0], vk[1] - W[1], vk[2] - W[2], F_vinc, T, lift, l0, l1, l2, drag, d0, d1, d2);
free(rk);
free(vk);
free(ak);
free(r_block);
free(v_block);
free(a_block);
free(r_diff);
free(v_diff);
free(a_diff);
fclose(trajectory);
fclose(debug);
//remove("a.out");
return 0;
}