/* * Copyright (C) 2020 Christopher J. Howard * * This file is part of Antkeeper source code. * * Antkeeper source code is free software: you can redistribute it and/or modify * it under the terms of the GNU General Public License as published by * the Free Software Foundation, either version 3 of the License, or * (at your option) any later version. * * Antkeeper source code is distributed in the hope that it will be useful, * but WITHOUT ANY WARRANTY; without even the implied warranty of * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the * GNU General Public License for more details. * * You should have received a copy of the GNU General Public License * along with Antkeeper source code. If not, see . */ #include "game/systems/solar-system.hpp" #include "game/astronomy/celestial-coordinates.hpp" #include "game/astronomy/celestial-mechanics.hpp" #include "game/astronomy/celestial-time.hpp" #include "game/components/orbit-component.hpp" #include "game/components/transform-component.hpp" #include using namespace ecs; static constexpr double seconds_per_day = 24.0 * 60.0 * 60.0; solar_system::solar_system(entt::registry& registry): entity_system(registry), julian_date(0.0), time_scale(1.0), latitude(0.0), longitude(0.0), altitude(0.0) {} void solar_system::update(double t, double dt) { // Add scaled timestep to Julian date set_julian_date(julian_date + (dt * time_scale) / seconds_per_day); const double ke_tolerance = 1e-6; const std::size_t ke_iterations = 10; ast::orbital_elements sun_elements; sun_elements.a = 1.0; sun_elements.ec = 0.016709; sun_elements.w = math::radians(282.9404); sun_elements.ma = math::radians(356.0470); sun_elements.i = math::radians(0.0); sun_elements.om = math::radians(0.0); const double j2k_day = julian_date - 2451545.0; const double j2k_century = (julian_date - 2451545.0) / 36525.0; sun_elements.ec += math::radians(-1.151e-9) * j2k_day; sun_elements.w += math::radians(4.70935e-5) * j2k_day; sun_elements.ma += math::radians(0.9856002585) * j2k_day; ast::orbital_state sun_ecliptic = ast::orbital_elements_to_state(sun_elements, ke_tolerance, ke_iterations); double3 sun_horizontal = ecliptic_to_horizontal * sun_ecliptic.r; sun_horizontal.z -= 4.25875e-5; double3 sun_spherical = ast::rectangular_to_spherical(sun_horizontal); double2 sun_az_el = {sun_spherical.z - math::pi, sun_spherical.y}; //std::cout << "new azel: " << math::degrees(sun_az_el.x) << ", " << math::degrees(sun_az_el.y) << std::endl; // Update horizontal (topocentric) positions of orbiting bodies registry.view().each( [&](auto entity, auto& orbit, auto& transform) { /* double a = orbit.a; double ec = orbit.ec; double w = orbit.w; double ma = orbit.ma; double i = orbit.i; double om = orbit.om; double3 ecliptic = ast::solve_kepler(a, ec, w, ma, i, om); double3 horizontal = ecliptic_to_horizontal * ecliptic; // Subtract Earth's radius (in AU), for positon of observer horizontal.z -= 4.25875e-5; // Transform into local right-handed coordinates double3 translation = ast::horizontal_to_right_handed * horizontal; double3x3 rotation = ast::horizontal_to_right_handed * ecliptic_to_horizontal; transform.local.translation = math::type_cast(translation); transform.local.rotation = math::type_cast(math::quaternion_cast(rotation)); */ }); } void solar_system::set_julian_date(double jd) { julian_date = jd; // Recalculate obliquity of the ecliptic ecl = ast::approx_ecliptic_obliquity(julian_date); // Recalculate LMST lmst = ast::jd_to_lmst(julian_date, longitude); // Recalculate ecliptic to horizontal transformation matrix ecliptic_to_horizontal = ast::ecliptic_to_horizontal(ecl, latitude, lmst); } void solar_system::set_time_scale(double scale) { time_scale = scale; } void solar_system::set_observer_location(double latitude, double longitude, double altitude) { this->latitude = latitude; this->longitude = longitude; this->altitude = altitude; // Recalculate LMST lmst = ast::jd_to_lmst(julian_date, longitude); // Recalculate ecliptic to horizontal transformation matrix ecliptic_to_horizontal = ast::ecliptic_to_horizontal(ecl, latitude, lmst); }