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- /*
- * 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 <http://www.gnu.org/licenses/>.
- */
-
- #ifndef ANTKEEPER_CELESTIAL_MECHANICS_HPP
- #define ANTKEEPER_CELESTIAL_MECHANICS_HPP
-
- #include "utility/fundamental-types.hpp"
-
- namespace ast
- {
-
- struct orbital_elements
- {
- double a; ///< Semi-major axis (km)
- double e; ///< Eccentricity
- double w; ///< Argument of periapsis (radians)
- double m; ///< Mean anomaly (radians)
- double i; ///< Inclination to the ecliptic (radians)
- double n; ///< Longitude of the ascending node (radians)
- };
-
- //constexpr orbital_elements j2k_orbit_moon = {384400.0, 0.0554, 318.15, 135.275.16, 125.08};
-
- struct orbital_state
- {
- double3 r; ///< Cartesian position
- double3 v; ///< Cartesian velocity
- };
-
- } // namespace ast
-
- #endif // ANTKEEPER_CELESTIAL_MECHANICS_HPP
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