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Merge pull request #7 from darioizzo/jpl_lp
Jpl lp
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// Copyright 2023, 2024 Dario Izzo ([email protected]), Francesco Biscani | ||
// ([email protected]) | ||
// | ||
// This file is part of the kep3 library. | ||
// | ||
// This Source Code Form is subject to the terms of the Mozilla | ||
// Public License v. 2.0. If a copy of the MPL was not distributed | ||
// with this file, You can obtain one at http://mozilla.org/MPL/2.0/. | ||
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#ifndef kep3_PLANET_JPL_LP_H | ||
#define kep3_PLANET_JPL_LP_H | ||
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#include <array> | ||
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#include <fmt/ostream.h> | ||
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#include <kep3/core_astro/constants.hpp> | ||
#include <kep3/detail/s11n.hpp> | ||
#include <kep3/detail/visibility.hpp> | ||
#include <kep3/epoch.hpp> | ||
#include <kep3/planet.hpp> | ||
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namespace kep3::udpla { | ||
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/// Solar System Planet (jpl simplified ephemerides) | ||
/** | ||
* This class allows to instantiate planets of | ||
* the solar system by referring to their common names. The ephemeris used | ||
* are low_precision ephemeris defined in the JPL pages: | ||
* https://ssd.jpl.nasa.gov/planets/approx_pos.html and valid for the timeframe | ||
* 1800AD - 2050 AD | ||
*/ | ||
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class kep3_DLL_PUBLIC jpl_lp { | ||
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std::array<double, 6> m_elements; | ||
std::array<double, 6> m_elements_dot; | ||
std::string m_name; | ||
double m_mu_central_body; | ||
double m_mu_self; | ||
double m_radius; | ||
double m_safe_radius; | ||
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friend class boost::serialization::access; | ||
template <typename Archive> void serialize(Archive &ar, unsigned) { | ||
ar &m_elements; | ||
ar &m_elements_dot; | ||
ar &m_name; | ||
ar &m_mu_central_body; | ||
ar &m_mu_self; | ||
ar &m_radius; | ||
ar &m_safe_radius; | ||
} | ||
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public: | ||
// Constructor | ||
explicit jpl_lp(const std::string & = "earth"); | ||
// Mandatory UDPLA methods | ||
[[nodiscard]] std::array<std::array<double, 3>, 2> eph(const epoch &) const; | ||
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// Optional UDPLA methods | ||
[[nodiscard]] std::string get_name() const; | ||
[[nodiscard]] double get_mu_central_body() const; | ||
[[nodiscard]] double get_mu_self() const; | ||
[[nodiscard]] double get_radius() const; | ||
[[nodiscard]] double get_safe_radius() const; | ||
[[nodiscard]] std::string get_extra_info() const; | ||
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// Other methods | ||
[[nodiscard]] std::array<double, 6> | ||
elements(const kep3::epoch & = kep3::epoch(), | ||
kep3::elements_type = kep3::elements_type::KEP_F) const; | ||
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private: | ||
[[nodiscard]] std::array<double, 6> | ||
_f_elements(const kep3::epoch & = kep3::epoch()) const; | ||
}; | ||
kep3_DLL_PUBLIC std::ostream &operator<<(std::ostream &, | ||
const kep3::udpla::jpl_lp &); | ||
} // namespace kep3::udpla | ||
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// fmt formatter redirecting to the stream operator | ||
template <> struct fmt::formatter<kep3::udpla::jpl_lp> : ostream_formatter {}; | ||
// necessary for serialization | ||
kep3_S11N_PLANET_EXPORT_KEY(kep3::udpla::jpl_lp); | ||
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#endif // KEP_TOOLBOX_PLANET_JPL_LP_H |
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// Copyright 2023, 2024 Dario Izzo ([email protected]), Francesco Biscani | ||
// ([email protected]) | ||
// | ||
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const kep3::udpla::keplerian &); | ||
} // namespace kep3::udpla | ||
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// fmt formatter redirecting to the stream operator | ||
template <> | ||
struct fmt::formatter<kep3::udpla::keplerian> : ostream_formatter {}; | ||
// necessary for serialization | ||
kep3_S11N_PLANET_EXPORT_KEY(kep3::udpla::keplerian); | ||
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#endif // kep3_EPOCH_H | ||
#endif // kep3_UDPLA_KEPLERIAN_H |
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// Copyright 2023, 2024 Dario Izzo ([email protected]), Francesco Biscani | ||
// ([email protected]) | ||
// | ||
// This file is part of the kep3 library. | ||
// | ||
// This Source Code Form is subject to the terms of the Mozilla | ||
// Public License v. 2.0. If a copy of the MPL was not distributed | ||
// with this file, You can obtain one at http://mozilla.org/MPL/2.0/. | ||
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#include "kep3/core_astro/eq2par2eq.hpp" | ||
#include "kep3/epoch.hpp" | ||
#include <cmath> | ||
#include <stdexcept> | ||
#include <unordered_map> | ||
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#include <boost/algorithm/string.hpp> | ||
#include <fmt/core.h> | ||
#include <fmt/ranges.h> | ||
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#include <kep3/core_astro/constants.hpp> | ||
#include <kep3/core_astro/convert_anomalies.hpp> | ||
#include <kep3/planet.hpp> | ||
#include <kep3/planets/jpl_lp.hpp> | ||
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namespace kep3::udpla { | ||
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// Data from: https://ssd.jpl.nasa.gov/planets/approx_pos.html | ||
// a,e,i,L,W,w | ||
// clang-format off | ||
static const std::array<double, 6> mercury_el = {0.38709927, 0.20563593, 7.00497902, 252.25032350, 77.45779628, 48.33076593}; | ||
static const std::array<double, 6> mercury_el_dot = {0.00000037, 0.00001906, -0.00594749, 149472.67411175, 0.16047689, -0.12534081}; | ||
static const std::array<double, 6> venus_el = {0.72333566, 0.00677672, 3.39467605, 181.97909950, 131.60246718, 76.67984255}; | ||
static const std::array<double, 6> venus_el_dot = {0.00000390, -0.00004107, -0.00078890, 58517.81538729, 0.00268329, -0.27769418}; | ||
static const std::array<double, 6> earth_moon_el = {1.00000261, 0.01671123, -0.00001531, 100.46457166, 102.93768193, 0.0}; | ||
static const std::array<double, 6> earth_moon_el_dot = {0.00000562, -0.00004392, -0.01294668, 35999.37244981, 0.32327364, 0.0}; | ||
static const std::array<double, 6> mars_el = {1.52371034, 0.09339410, 1.84969142, -4.55343205, -23.94362959, 49.55953891}; | ||
static const std::array<double, 6> mars_el_dot = {0.00001847, 0.00007882, -0.00813131, 19140.30268499, 0.44441088, -0.29257343}; | ||
static const std::array<double, 6> jupiter_el = {5.20288700, 0.04838624, 1.30439695, 34.39644051, 14.72847983, 100.47390909}; | ||
static const std::array<double, 6> jupiter_el_dot = {-0.00011607, -0.00013253, -0.00183714, 3034.74612775, 0.21252668, 0.20469106}; | ||
static const std::array<double, 6> saturn_el = {9.53667594, 0.05386179, 2.48599187, 49.95424423, 92.59887831, 113.66242448}; | ||
static const std::array<double, 6> saturn_el_dot = {-0.00125060, -0.00050991, 0.00193609, 1222.49362201, -0.41897216, -0.28867794}; | ||
static const std::array<double, 6> uranus_el = {19.18916464, 0.04725744, 0.77263783, 313.23810451, 170.95427630, 74.01692503}; | ||
static const std::array<double, 6> uranus_el_dot = {-0.00196176, -0.00004397, -0.00242939, 428.48202785, 0.40805281, 0.04240589}; | ||
static const std::array<double, 6> neptune_el = {30.06992276, 0.00859048, 1.77004347, -55.12002969, 44.96476227, 131.78422574}; | ||
static const std::array<double, 6> neptune_el_dot = {0.00026291, 0.00005105, 0.00035372, 218.45945325, -0.32241464, -0.00508664}; | ||
// clang-format on | ||
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jpl_lp::jpl_lp(const std::string &name) | ||
: m_elements(), m_elements_dot(), m_name(name), | ||
m_mu_central_body(kep3::MU_SUN) { | ||
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// Cannot be marked const as operator[] is not and we use it. | ||
static std::unordered_map<std::string, int> mapped_planets = { | ||
{"mercury", 1}, {"venus", 2}, {"earth", 3}, | ||
{"mars", 4}, {"jupiter", 5}, {"saturn", 6}, | ||
{"uranus", 7}, {"neptune", 8}, {"pluto", 9}}; | ||
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boost::algorithm::to_lower(m_name); | ||
switch (mapped_planets[m_name]) { | ||
case (1): { | ||
m_elements = mercury_el; | ||
m_elements_dot = mercury_el_dot; | ||
m_radius = 2440000.; | ||
m_safe_radius = 1.1 * m_radius; | ||
m_mu_self = 22032e9; | ||
} break; | ||
case (2): { | ||
m_elements = venus_el; | ||
m_elements_dot = venus_el_dot; | ||
m_radius = 6052000.; | ||
m_safe_radius = 1.1 * m_radius; | ||
m_mu_self = 324859e9; | ||
} break; | ||
case (3): { | ||
m_elements = earth_moon_el; | ||
m_elements_dot = earth_moon_el_dot; | ||
m_radius = 6378000.; | ||
m_safe_radius = 1.1 * m_radius; | ||
m_mu_self = 398600.4418e9; | ||
} break; | ||
case (4): { | ||
m_elements = mars_el; | ||
m_elements_dot = mars_el_dot; | ||
m_radius = 3397000.; | ||
m_safe_radius = 1.1 * m_radius; | ||
m_mu_self = 42828e9; | ||
} break; | ||
case (5): { | ||
m_elements = jupiter_el; | ||
m_elements_dot = jupiter_el_dot; | ||
m_radius = 71492000.; | ||
m_safe_radius = 9. * m_radius; | ||
m_mu_self = 126686534e9; | ||
} break; | ||
case (6): { | ||
m_elements = saturn_el; | ||
m_elements_dot = saturn_el_dot; | ||
m_radius = 60330000.; | ||
m_safe_radius = 1.1 * m_radius; | ||
m_mu_self = 37931187e9; | ||
} break; | ||
case (7): { | ||
m_elements = uranus_el; | ||
m_elements_dot = uranus_el_dot; | ||
m_radius = 25362000.; | ||
m_safe_radius = 1.1 * m_radius; | ||
m_mu_self = 5793939e9; | ||
} break; | ||
case (8): { | ||
m_elements = neptune_el; | ||
m_elements_dot = neptune_el_dot; | ||
m_radius = 24622000.; | ||
m_safe_radius = 1.1 * m_radius; | ||
m_mu_self = 6836529e9; | ||
} break; | ||
default: { | ||
throw std::logic_error("unknown planet name: "); | ||
} | ||
} | ||
} | ||
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// Computes the kep3::KEP_F elements (osculating with true anomaly) at epoch. | ||
std::array<double, 6> jpl_lp::_f_elements(const kep3::epoch &ep) const { | ||
double mjd2000 = ep.mjd2000(); | ||
if (mjd2000 <= -73048.0 || mjd2000 >= 18263.0) { | ||
throw std::domain_error("Low precision Ephemeris are only valid in the " | ||
"range range [1800-2050]"); | ||
} | ||
// algorithm from https://ssd.jpl.nasa.gov/planets/approx_pos.html accessed | ||
// 2023. | ||
std::array<double, 6> elements_updated{}, elements_f{}; | ||
double dt = mjd2000 / 36525.; // Number of centuries passed since J2000.0 | ||
for (unsigned int i = 0; i < 6; ++i) { | ||
elements_updated[i] = (m_elements[i] + m_elements_dot[i] * dt); | ||
} | ||
elements_f[0] = elements_updated[0] * kep3::AU; | ||
elements_f[1] = elements_updated[1]; | ||
elements_f[2] = elements_updated[2] * kep3::DEG2RAD; | ||
elements_f[3] = elements_updated[5] * kep3::DEG2RAD; | ||
elements_f[4] = (elements_updated[4] - elements_updated[5]) * kep3::DEG2RAD; | ||
elements_f[5] = (elements_updated[3] - elements_updated[4]) * kep3::DEG2RAD; | ||
elements_f[5] = kep3::m2f(elements_f[5], elements_f[1]); | ||
return elements_f; | ||
} | ||
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std::array<std::array<double, 3>, 2> jpl_lp::eph(const epoch &ep) const { | ||
auto elements_f = _f_elements(ep); | ||
return par2ic(elements_f, get_mu_central_body()); | ||
} | ||
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std::array<double, 6> jpl_lp::elements(const kep3::epoch &ep, | ||
kep3::elements_type el_type) const { | ||
auto elements = _f_elements(ep); | ||
switch (el_type) { | ||
case kep3::elements_type::KEP_F: | ||
break; | ||
case kep3::elements_type::KEP_M: | ||
elements[5] = kep3::f2m(elements[5], elements[1]); | ||
break; | ||
case kep3::elements_type::MEQ: | ||
elements = kep3::par2eq(elements, false); | ||
break; | ||
case kep3::elements_type::MEQ_R: | ||
elements = kep3::par2eq(elements, true); | ||
break; | ||
default: | ||
throw std::logic_error("You should not go here!"); | ||
} | ||
return elements; | ||
} | ||
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std::string jpl_lp::get_name() const { return m_name; } | ||
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double jpl_lp::get_mu_central_body() const { return m_mu_central_body; } | ||
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double jpl_lp::get_mu_self() const { return m_mu_self; } | ||
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double jpl_lp::get_radius() const { return m_radius; } | ||
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double jpl_lp::get_safe_radius() const { return m_safe_radius; } | ||
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std::string jpl_lp::get_extra_info() const { | ||
kep3::epoch ep{0., kep3::epoch::MJD2000}; | ||
auto par = elements(ep); | ||
auto pos_vel = eph(ep); | ||
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std::string retval = | ||
fmt::format("\nLow-precision planet elements: \n") + | ||
fmt::format("Semi major axis (AU): {}\n", par[0] / kep3::AU) + | ||
fmt::format("Eccentricity: {}\n", par[1]) + | ||
fmt::format("Inclination (deg.): {}\n", par[2] * kep3::RAD2DEG) + | ||
fmt::format("Big Omega (deg.): {}\n", par[3] * kep3::RAD2DEG) + | ||
fmt::format("Small omega (deg.): {}\n", par[4] * kep3::RAD2DEG) + | ||
fmt::format("True anomly (deg.): {}\n", par[5] * kep3::RAD2DEG); | ||
retval += fmt::format("Mean anomly (deg.): {}\n", | ||
kep3::f2m(par[5], par[1]) * kep3::RAD2DEG); | ||
retval += | ||
fmt::format("Elements reference epoch (MJD2000): {}\n", ep.mjd2000()) + | ||
fmt::format("Elements reference epoch (date): {}\n", ep) + | ||
fmt::format("r at ref. = {}\n", pos_vel[0]) + | ||
fmt::format("v at ref. = {}\n", pos_vel[1]); | ||
return retval; | ||
} | ||
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std::ostream &operator<<(std::ostream &os, const kep3::udpla::jpl_lp &udpla) { | ||
os << udpla.get_extra_info() << std::endl; | ||
return os; | ||
} | ||
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} // namespace kep3::udpla | ||
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kep3_S11N_PLANET_IMPLEMENT(kep3::udpla::jpl_lp) |
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