...

Undisturbed_movement/Disturbed_movement.cpp

@@ -14,26 +14,6 @@ int main()
 {
     Kepler_elements_orbit element{26559.81038, 0.01203, 56.6024, 106.997, 53.2777, 154.03184};
     satellite_parameters param{ 1,3,1.5 };
-//    Matrix a{ 3, 1, {1000, 1000, 1000} };
-//    Matrix b{ 3, 1, {100, 100, 100} };
-//    
-//    Matrix c{ 3, 1, {5000, 5000, 5000} };
-//    Matrix d{ 3, 1, {1000, 1, 1000} };
-//    
-//    Moon m_moon{ 59777.67019 };
-//    Sun m_sun{ 59777.67019 };
-//    Earth m_earth { 59777.67019, c};
-////    std::vector<Satellite> {};
-//    
-//    
-//    Satellite m_k{ 59777.67019, param, c, d, &m_moon, &m_sun, &m_earth };
-//    Satellite two{ 59777.67019, param, element, &m_moon, &m_sun, &m_earth };
-//    //m_k.integration_step(59777.77019);
-//    two.integration_step(59777.77019);
-//    std::cout << two.getId();
-
-    
-
     modulation({ 2022, 07,19,18,20,00 }, 0.00011, false, { 2022, 07,19,18,30,00 });
     return 0;
 }