geocentric_position_v = SGGeoc::fromCart(cartesian_position_v);
euler_angles_v = SGVec3d::zeros();
- mass=i_xx=i_yy=i_zz=i_xz=0;
nlf=0;
v_rel_wind=v_true_kts=0;
v_ground_speed=v_equiv_kts=0;
SG_LOG(SG_FLIGHT,SG_INFO,"geodetic_position_v: " << geodetic_position_v);
SG_LOG(SG_FLIGHT,SG_INFO,"euler_angles_v: " << euler_angles_v);
- SG_LOG(SG_FLIGHT,SG_INFO,"mass: " << mass );
- SG_LOG(SG_FLIGHT,SG_INFO,"i_xx: " << i_xx );
- SG_LOG(SG_FLIGHT,SG_INFO,"i_yy: " << i_yy );
- SG_LOG(SG_FLIGHT,SG_INFO,"i_zz: " << i_zz );
- SG_LOG(SG_FLIGHT,SG_INFO,"i_xz: " << i_xz );
SG_LOG(SG_FLIGHT,SG_INFO,"nlf: " << nlf );
SG_LOG(SG_FLIGHT,SG_INFO,"v_rel_wind: " << v_rel_wind );
SG_LOG(SG_FLIGHT,SG_INFO,"v_true_kts: " << v_true_kts );