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#define _USE_MATH_DEFINES
#include "orbit.h"
Orbit::Orbit(elements_orbit input_elements) : m_elements{ input_elements } {
calculate_const_elements_ellipse();
log_coordinates.open("log_coordinates.txt");
log_coordinates << m_elements << "\n--------------------------------\n" << m_const_ellipse
<< "\n--------------------------------\n";
};
int Orbit::calculate_E(int accuracy) {
double epsilon = pow(10, -accuracy);
double buffer_Ek{ m_variable_ellipse.M };
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double buffer_Ek1 = 0;
while (std::abs(buffer_Ek1 - buffer_Ek) > epsilon) {
buffer_Ek1 = m_variable_ellipse.M + m_elements.e * sin(buffer_Ek);
buffer_Ek = buffer_Ek1;
}
m_variable_ellipse.E = buffer_Ek;
return 1;
}
int Orbit::calculate_const_elements_ellipse() {
m_const_ellipse.r_p = m_elements.p / (1 + m_elements.e);
m_const_ellipse.r_a = m_elements.p / (1 - m_elements.e);
m_const_ellipse.a = (m_const_ellipse.r_p + m_const_ellipse.r_a) / 2;
m_const_ellipse.b = sqrt(m_const_ellipse.r_p + m_const_ellipse.r_a);
m_const_ellipse.abs_c = sqrt(m_elements.p * gravitational_parameter_Earth);
m_const_ellipse.n = sqrt(gravitational_parameter_Earth / pow(m_const_ellipse.a, 3));
m_const_ellipse.T = 2 * M_PI * sqrt(pow(m_const_ellipse.a, 3) / gravitational_parameter_Earth);
return 1;
}
int Orbit::calculate_varible_elements_ellipse(double current_time) {
log_coordinates << std::setprecision(20) << current_time << "\n";
m_variable_ellipse.M = m_const_ellipse.n * (current_time - m_elements.tau);
calculate_E(4);
m_variable_ellipse.nu = 2 * atan(sqrt((1 + m_elements.e) / (1 + m_elements.e)) * tan(m_variable_ellipse.E / 2));
m_variable_ellipse.r = m_elements.p / (1 + m_elements.e * cos(m_variable_ellipse.nu));
m_variable_ellipse.u = m_elements.omega + m_variable_ellipse.nu;
m_variable_ellipse.Vr= sqrt(gravitational_parameter_Earth * m_elements.p) * m_elements.e * sin(m_variable_ellipse.nu);
m_variable_ellipse.dnu = m_const_ellipse.abs_c / pow(m_variable_ellipse.r, 2);
return 1;
}
int Orbit::calculate_coordinates() {
m_coordinates.x = m_variable_ellipse.r * (cos(m_variable_ellipse.u) * cos(m_elements.precession) -
sin(m_variable_ellipse.u) * sin(m_elements.precession) * cos(m_elements.nutation));
m_coordinates.y = m_variable_ellipse.r * (cos(m_variable_ellipse.u) * sin(m_elements.precession) +
sin(m_variable_ellipse.u) * cos(m_elements.precession) * cos(m_elements.nutation));
m_coordinates.z = m_variable_ellipse.r * sin(m_variable_ellipse.u) * sin(m_elements.nutation);
return 0;
}
int Orbit::calculate_speed_components() {
m_speed_components.v_x = m_variable_ellipse.Vr * m_coordinates.x / m_variable_ellipse.r -
m_variable_ellipse.r * (sin(m_variable_ellipse.u) * cos(m_elements.precession) +
cos(m_variable_ellipse.u) * sin(m_elements.precession) * cos(m_elements.nutation))*m_variable_ellipse.dnu;
m_speed_components.v_y = m_variable_ellipse.Vr * m_coordinates.y / m_variable_ellipse.r -
m_variable_ellipse.r * (sin(m_variable_ellipse.u) * sin(m_elements.precession) -
cos(m_variable_ellipse.u) * cos(m_elements.precession) * cos(m_elements.nutation)) * m_variable_ellipse.dnu;
m_speed_components.v_z = m_variable_ellipse.Vr * m_coordinates.z / m_variable_ellipse.r +
m_variable_ellipse.r * cos(m_variable_ellipse.u) * sin(m_elements.nutation) * m_variable_ellipse.dnu;
return 0;
}
int Orbit::modulation() {
calculate_varible_elements_ellipse(m_time.getCurrent_US());
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calculate_coordinates();
calculate_speed_components();
log_coordinates << m_coordinates << "\n" << m_speed_components << "\n--------------------------------\n";
return 0;
}
std::ostream& operator<<(std::ostream& out, const elements_orbit& i_elements_orbit)
{
out << "Focal parameter = " << i_elements_orbit.p << " || "
<< "eccentricity of the orbit = " << i_elements_orbit.e << " || "
<< "longitude of the ascending node = " << i_elements_orbit.precession << "\n"
<< "inclination of the orbit = " << i_elements_orbit.nutation << " || "
<< "the perigee latitude argument" << i_elements_orbit.omega << " || "
<< "tau = "<< i_elements_orbit.tau;
return out;
}
std::ofstream& operator<<(std::ofstream& out, const elements_orbit& i_elements_orbit)
{
out << "Focal parameter = " << i_elements_orbit.p << " || "
<< "eccentricity of the orbit = " << i_elements_orbit.e << " || "
<< "longitude of the ascending node = " << i_elements_orbit.precession << "\n"
<< "inclination of the orbit = " << i_elements_orbit.nutation << " || "
<< "the perigee latitude argument" << i_elements_orbit.omega << " || "
<< "tau = " << i_elements_orbit.tau;
return out;
}
std::ostream& operator <<(std::ostream& out, const const_elements_ellipse_orbite& i_const_elements_ellipse_orbite) {
out << "Smallest distance = " << i_const_elements_ellipse_orbite.r_p << " || "
<< "the largest distance = " << i_const_elements_ellipse_orbite.r_a << " || "
<< "major semiaxis = " << i_const_elements_ellipse_orbite.a << "\n"
<< "minor semiaxis = " << i_const_elements_ellipse_orbite.b << " || "
<< "constant vector of areas = " << i_const_elements_ellipse_orbite.abs_c << " || "
<< "constant angular velocity" << i_const_elements_ellipse_orbite.n << "\n"
<< "orbit period" << i_const_elements_ellipse_orbite.T;
return out;
}
std::ofstream& operator <<(std::ofstream& out, const const_elements_ellipse_orbite& i_const_elements_ellipse_orbite) {
out << "Smallest distance = " << i_const_elements_ellipse_orbite.r_p << " || "
<< "the largest distance = " << i_const_elements_ellipse_orbite.r_a << " || "
<< "major semiaxis = " << i_const_elements_ellipse_orbite.a << "\n"
<< "minor semiaxis = " << i_const_elements_ellipse_orbite.b << " || "
<< "constant vector of areas = " << i_const_elements_ellipse_orbite.abs_c << " || "
<< "constant angular velocity" << i_const_elements_ellipse_orbite.n << "\n"
<< "orbit period" << i_const_elements_ellipse_orbite.T;
return out;
}
std::ostream& operator <<(std::ostream& out, const variable_elements_ellipse_orbit& i_variable_elements_ellipse_orbit) {
out << "Average anomaly = " << i_variable_elements_ellipse_orbit.M << " || "
<< "Eccentric anomaly = " << i_variable_elements_ellipse_orbit.E << " || "
<< "True anomaly = " << i_variable_elements_ellipse_orbit.nu << " || "
<< "radius-vector" << i_variable_elements_ellipse_orbit.r << "\n"
<< "satellite latitude argument = " << i_variable_elements_ellipse_orbit.u << " || "
<< "angular velocity = " << i_variable_elements_ellipse_orbit.dnu << " || "
<< "radial velocity projection = " << i_variable_elements_ellipse_orbit.Vr;
return out;
}
std::ofstream& operator <<(std::ofstream& out, const variable_elements_ellipse_orbit& i_variable_elements_ellipse_orbit) {
out << "Average anomaly = " << i_variable_elements_ellipse_orbit.M << " || "
<< "Eccentric anomaly = " << i_variable_elements_ellipse_orbit.E << " || "
<< "True anomaly = " << i_variable_elements_ellipse_orbit.nu << " || "
<< "radius-vector" << i_variable_elements_ellipse_orbit.r << "\n"
<< "satellite latitude argument = " << i_variable_elements_ellipse_orbit.u << " || "
<< "angular velocity = " << i_variable_elements_ellipse_orbit.dnu << " || "
<< "radial velocity projection = " << i_variable_elements_ellipse_orbit.Vr;
return out;
}
std::ostream& operator <<(std::ostream& out, const coordinates& i_coordinates) {
out << "x = " << i_coordinates.x << " || "
<< "y = " << i_coordinates.y << " || "
<< "z = " << i_coordinates.z;
return out;
}
std::ofstream& operator <<(std::ofstream& out, const coordinates& i_coordinates) {
out << "x = " << i_coordinates.x << " || "
<< "y = " << i_coordinates.y << " || "
<< "z = " << i_coordinates.z;
return out;
}
std::ostream& operator <<(std::ostream& out, const speed_components& i_speed_components) {
out << "V_x = " << i_speed_components.v_x << " || "
<< "V_y = " << i_speed_components.v_y << " || "
<< "V_z = " << i_speed_components.v_z;
return out;
};
std::ofstream& operator <<(std::ofstream& out, const speed_components& i_speed_components) {
out << "V_x = " << i_speed_components.v_x << " || "
<< "V_y = " << i_speed_components.v_y << " || "
<< "V_z = " << i_speed_components.v_z;
return out;
};
std::ostream& operator <<(std::ostream& out, const Orbit& out_orbit) {
out << "elements_orbit\n" << out_orbit.m_elements << "\n--------------------------------\n"
<< "const_elements_ellipse_orbite\n" << out_orbit.m_const_ellipse << "\n--------------------------------\n"
<< "variable_elements_ellipse_orbit\n" << out_orbit.m_variable_ellipse << "\n--------------------------------\n";
return out;
};
std::ofstream& operator <<(std::ofstream& out, const Orbit& out_orbit) {
out << "elements_orbit\n" << out_orbit.m_elements << "\n--------------------------------\n"
<< "const_elements_ellipse_orbite\n" << out_orbit.m_const_ellipse << "\n--------------------------------\n"
<< "variable_elements_ellipse_orbit\n" << out_orbit.m_variable_ellipse << "\n--------------------------------\n";
return out;
};