coordinates_examples.cpp

Focused examples for creating and converting typed coordinates.

Focused examples for creating and converting typed coordinates.Usage: cmake –build build-make –target coordinates_examples ./build-make/coordinates_examples

 
#include <siderust/siderust.hpp>
 
#include <cstdio>
 
using namespace siderust;
using namespace qtty::literals;
 
static void geodetic_and_ecef_example() {
    std::printf("1) Geodetic -> ECEF cartesian\n");
 
    Geodetic obs(-17.8890, 28.7610, 2396.0);
    auto     ecef    = obs.to_cartesian();
    auto     ecef_km = obs.to_cartesian<qtty::Kilometer>();
 
    std::printf("   Geodetic lon=%.4f deg lat=%.4f deg h=%.1f m\n",
                obs.lon.value(), obs.lat.value(), obs.height.value());
    std::printf("   ECEF x=%.2f m y=%.2f m z=%.2f m\n\n",
                ecef.x().value(), ecef.y().value(), ecef.z().value());
    std::printf("   ECEF x=%.2f km y=%.2f km z=%.2f km\n\n",
                ecef_km.x().value(), ecef_km.y().value(), ecef_km.z().value());
}
 
static void spherical_direction_example() {
    std::printf("2) Spherical direction frame conversions\n");
 
    spherical::direction::ICRS vega_icrs(279.23473, 38.78369);
    auto                       jd = JulianDate::from_utc({2026, 7, 15, 22, 0, 0});
 
    auto ecl    = vega_icrs.to<frames::EclipticMeanJ2000>(jd);
    auto eq_mod = vega_icrs.to<frames::EquatorialMeanOfDate>(jd);
    auto hor    = vega_icrs.to_horizontal(jd, ROQUE_DE_LOS_MUCHACHOS);
 
    std::printf("   ICRS RA=%.5f Dec=%.5f\n", vega_icrs.ra().value(), vega_icrs.dec().value());
    std::printf("   Ecliptic lon=%.5f lat=%.5f\n", ecl.lon().value(), ecl.lat().value());
    std::printf("   Equatorial(MOD) RA=%.5f Dec=%.5f\n", eq_mod.ra().value(), eq_mod.dec().value());
    std::printf("   Horizontal az=%.5f alt=%.5f\n\n", hor.az().value(), hor.alt().value());
}
 
static void spherical_position_example() {
    std::printf("3) Spherical position + extracting direction\n");
 
    spherical::position::ICRS<qtty::Meter> target(
        120.0_deg, -25.0_deg, 2.0e17_m);
    auto dir = target.direction();
 
    std::printf("   Position RA=%.2f Dec=%.2f dist=%.3e m\n",
                target.ra().value(), target.dec().value(), target.distance().value());
    std::printf("   Direction-only RA=%.2f Dec=%.2f\n\n",
                dir.ra().value(), dir.dec().value());
}
 
static void cartesian_and_units_example() {
    std::printf("4) Cartesian coordinate creation + unit conversion\n");
 
    cartesian::Direction<frames::ICRS>                             axis_x(1.0, 0.0, 0.0);
    cartesian::position::EclipticMeanJ2000<qtty::AstronomicalUnit> sample_helio_au(1.0, 0.25, -0.1);
 
    auto x_km = sample_helio_au.x().to<qtty::Kilometer>();
    auto y_km = sample_helio_au.y().to<qtty::Kilometer>();
 
    std::printf("   Direction<ICRS> x=%.1f y=%.1f z=%.1f\n", axis_x.x, axis_x.y, axis_x.z);
    std::printf("   Position<Heliocentric,Ecl,AU> x=%.3f AU y=%.3f AU z=%.3f AU\n",
                sample_helio_au.x().value(), sample_helio_au.y().value(), sample_helio_au.z().value());
    std::printf("   Same position in km x=%.2f y=%.2f\n\n", x_km.value(), y_km.value());
}
 
static void ephemeris_typed_example() {
    std::printf("5) Typed ephemeris coordinates\n");
 
    auto jd    = JulianDate::J2000();
    auto earth = ephemeris::earth_heliocentric(jd); // cartesian::position::EclipticMeanJ2000<qtty::AstronomicalUnit>
    auto moon  = ephemeris::moon_geocentric(jd);    // cartesian::position::MoonGeocentric<qtty::Kilometer>
 
    std::printf("   Earth heliocentric (AU) x=%.8f y=%.8f z=%.8f\n",
                earth.x().value(), earth.y().value(), earth.z().value());
    std::printf("   Moon geocentric (km) x=%.3f y=%.3f z=%.3f\n\n",
                moon.x().value(), moon.y().value(), moon.z().value());
}
 
int main() {
    std::printf("=== Coordinate Creation & Conversion Examples ===\n\n");
 
    geodetic_and_ecef_example();
    spherical_direction_example();
    spherical_position_example();
    cartesian_and_units_example();
    ephemeris_typed_example();
 
    std::printf("Done.\n");
    return 0;
}