void magnetic_field_estimator(vector v_B_o)
{
float time_in_years = 2015 + (float)seconds_since_pivot / SECONDS_IN_YEAR;
vector v_temp, v_r_lla, v_B_ned, v_B_eci;
eci2ecef(v_r, v_temp);
ecef2lla(v_temp, v_r_lla);// LLA is need
///* Save LLA vector for use in communications check routine
copy_vector(v_r_lla, v_sat);// why is this required when ,lat long alt coming from GPS
igrf(v_r_lla, time_in_years, 8, v_B_ned);// need to check at the end
ned2ecef(v_B_ned, v_r_lla, v_temp);
ecef2eci(v_temp, v_B_eci);
eci2orbit(v_r, v_v, v_B_eci, v_B_o);
scalar_into_vector(v_B_o, 1e-9); // igrf gives in nT
int8_t sen,sen1;
int16_t st;
/*for (int i=0;i<3;i=i+1)
{
//sen = ((int8_t)((lambda))/2);
st =(int16_t)(v_B_eci[i]/10);
sen = (int8_t)st;
sen1 = (int8_t)(st>>8);
transmit_UART0(sen);
transmit_UART0(sen1);
}*/
}
void magnetic_field_estimator(vector v_B_o)
{
float time_in_years = 2010 + (float)seconds_since_pivot / SECONDS_IN_YEAR;
vector v_temp, v_r_lla, v_B_ned, v_B_eci;
eci2ecef(v_r, v_temp);
ecef2lla(v_temp, v_r_lla);
igrf(v_r_lla, time_in_years, 8, v_B_ned);
ned2ecef(v_B_ned, v_r_lla, v_temp);
ecef2eci(v_temp, v_B_eci);
eci2orbit(v_r, v_v, v_B_eci, v_B_o);
scalar_into_vector(v_B_o, 1e-9);
}
void magnetic_field_estimator(vector v_B_o)
{
float time_in_years = 2010 + (float)seconds_since_pivot / SECONDS_IN_YEAR;
vector v_temp, v_r_lla, v_B_ned, v_B_eci;
eci2ecef(v_r, v_temp);
ecef2lla(v_temp, v_r_lla);
///* Save LLA vector for use in communications check routine
copy_vector(v_r_lla, v_sat);
igrf(v_r_lla, time_in_years, 8, v_B_ned);
ned2ecef(v_B_ned, v_r_lla, v_temp);
ecef2eci(v_temp, v_B_eci);
eci2orbit(v_r, v_v, v_B_eci, v_B_o);
scalar_into_vector(v_B_o, 1e-9);
}
