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Add Orrery example

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Uses sprites for flicker free animation
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Bodmer
2020-10-20 00:53:08 +01:00
parent 482e559b26
commit 0d31c9f1a5
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// Display an Orrery
// Works for all display sizes but 320x480 minimum size recommended
// Whole planet orbits only visible in 480 x 800 display
// Flicker free sprite example for TFT_eSPI:
// https://github.com/Bodmer/TFT_eSPI
// Sketch coded by Bodmer
// Uses astronomy engine created by Don Cross
#include <TFT_eSPI.h> // Hardware-specific library
TFT_eSPI tft = TFT_eSPI(); // Invoke library
TFT_eSprite img = TFT_eSprite(&tft); // Sprite class
#define sunX tft.width()/2
#define sunY tft.height()/2
uint16_t orb_inc;
uint16_t planet_r;
#include <stdio.h>
#include "astronomy.h"
#define TIME_TEXT_BYTES 25
astro_time_t astro_time;
uint16_t grey;
static const astro_body_t body[] = {
BODY_SUN, BODY_MERCURY, BODY_VENUS, BODY_EARTH, BODY_MARS,
BODY_JUPITER, BODY_SATURN, BODY_URANUS, BODY_NEPTUNE
};
static const uint16_t bodyColour[] = {
TFT_YELLOW, TFT_DARKGREY, TFT_ORANGE, TFT_BLUE, TFT_RED,
TFT_GOLD, TFT_BROWN, TFT_DARKCYAN, TFT_CYAN
};
// =========================================================================
// Setup
// =========================================================================
void setup() {
Serial.begin(115200);
tft.begin();
tft.setRotation(1);
tft.fillScreen(TFT_BLACK);
// Test with smaller display sizes
//tft.setViewport(10,10,160,128);
//tft.setViewport(10,10,320,240);
//tft.setViewport(10,10,480,320);
//tft.frameViewport(TFT_GREEN, -1);
img.createSprite(19, 19);
grey = tft.color565(30, 30, 30);
astro_time = Astronomy_MakeTime(2020, 10, 16, 19, 31, 0) ;
tft.fillCircle(sunX, sunY, 10, TFT_YELLOW);
// i initialised to 1 so Sun is skipped
for (int i = 1; i < sizeof(body) / sizeof(body[0]); ++i)
{
tft.drawCircle(sunX, sunY, i * 28, grey);
}
}
// =========================================================================
// Loop
// =========================================================================
void loop() {
uint32_t dt = millis();
plot_planets();
showTime(astro_time);
// Add time increment (more than 0.6 days will lead to stray pixel on screen
// due to the way previous object images are erased)
astro_time = Astronomy_AddDays(astro_time, 0.25); // 0.25 day (6 hour) increment
dt = millis()-dt;
//Serial.println(dt);
//delay(1000);
}
// =========================================================================
// Get coordinates of end of a vector, pivot at x,y, length r, angle a
// =========================================================================
// Coordinates are returned to caller via the xp and yp pointers
#define DEG2RAD 0.0174532925
void getCoord(int x, int y, int *xp, int *yp, int r, float a)
{
float sx1 = cos( -a * DEG2RAD );
float sy1 = sin( -a * DEG2RAD );
*xp = sx1 * r + x;
*yp = sy1 * r + y;
}
// =========================================================================
// Convert astronomical time to UTC and display
// =========================================================================
void showTime(astro_time_t time)
{
astro_status_t status;
char text[TIME_TEXT_BYTES];
status = Astronomy_FormatTime(time, TIME_FORMAT_SECOND, text, sizeof(text));
if (status != ASTRO_SUCCESS)
{
fprintf(stderr, "\nFATAL(PrintTime): status %d\n", status);
exit(1);
}
tft.drawString(text, 0, 0, 2);
}
// =========================================================================
// Plot planet positions as an Orrery
// =========================================================================
int plot_planets(void)
{
astro_angle_result_t ang;
int i;
int num_bodies = sizeof(body) / sizeof(body[0]);
// i initialised to 1 so Sun is skipped
for (i = 1; i < num_bodies; ++i)
{
ang = Astronomy_EclipticLongitude(body[i], astro_time);
int x1 = 0; // getCoord() will update these
int y1 = 0;
getCoord(0, 0, &x1, &y1, i * 28, ang.angle); // Get x1 ,y1
img.fillSprite(TFT_TRANSPARENT);
img.fillCircle(9, 9, 9, TFT_BLACK);
img.drawCircle(9 - x1, 9 - y1, i * 28, grey);
img.fillCircle(9, 9, 5, bodyColour[i]);
img.pushSprite(sunX + x1 - 9, sunY + y1 - 9, TFT_TRANSPARENT);
if (body[i] == BODY_EARTH)
{
astro_angle_result_t mang = Astronomy_LongitudeFromSun(BODY_MOON, astro_time);
int xm = 0;
int ym = 0;
getCoord(x1, y1, &xm, &ym, 15, 180 + ang.angle + mang.angle); // Get x1 ,y1
img.fillSprite(TFT_TRANSPARENT);
img.fillCircle(9, 9, 7, TFT_BLACK);
img.drawCircle(9 - xm, 9 - ym, i * 28, grey);
img.fillCircle(9, 9, 2, TFT_WHITE);
img.pushSprite(sunX + xm - 9, sunY + ym - 9, TFT_TRANSPARENT);
}
}
return 0;
}

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/*
Astronomy Engine for C/C++.
https://github.com/cosinekitty/astronomy
MIT License
Copyright (c) 2019-2020 Don Cross <cosinekitty@gmail.com>
Permission is hereby granted, free of charge, to any person obtaining a copy
of this software and associated documentation files (the "Software"), to deal
in the Software without restriction, including without limitation the rights
to use, copy, modify, merge, publish, distribute, sublicense, and/or sell
copies of the Software, and to permit persons to whom the Software is
furnished to do so, subject to the following conditions:
The above copyright notice and this permission notice shall be included in all
copies or substantial portions of the Software.
THE SOFTWARE IS PROVIDED "AS IS", WITHOUT WARRANTY OF ANY KIND, EXPRESS OR
IMPLIED, INCLUDING BUT NOT LIMITED TO THE WARRANTIES OF MERCHANTABILITY,
FITNESS FOR A PARTICULAR PURPOSE AND NONINFRINGEMENT. IN NO EVENT SHALL THE
AUTHORS OR COPYRIGHT HOLDERS BE LIABLE FOR ANY CLAIM, DAMAGES OR OTHER
LIABILITY, WHETHER IN AN ACTION OF CONTRACT, TORT OR OTHERWISE, ARISING FROM,
OUT OF OR IN CONNECTION WITH THE SOFTWARE OR THE USE OR OTHER DEALINGS IN THE
SOFTWARE.
*/
#ifndef __ASTRONOMY_H
#define __ASTRONOMY_H
#include <stddef.h> /* for size_t */
#ifdef __cplusplus
extern "C" {
#endif
/*---------- types ----------*/
/**
* @brief Indicates success/failure of an Astronomy Engine function call.
*/
typedef enum
{
ASTRO_SUCCESS, /**< The operation was successful. */
ASTRO_NOT_INITIALIZED, /**< A placeholder that can be used for data that is not yet initialized. */
ASTRO_INVALID_BODY, /**< The celestial body was not valid. Different sets of bodies are supported depending on the function. */
ASTRO_NO_CONVERGE, /**< A numeric solver failed to converge. This should not happen unless there is a bug in Astronomy Engine. */
ASTRO_BAD_TIME, /**< The provided date/time is outside the range allowed by this function. */
ASTRO_BAD_VECTOR, /**< Vector magnitude is too small to be normalized into a unit vector. */
ASTRO_SEARCH_FAILURE, /**< Search was not able to find an ascending root crossing of the function in the specified time interval. */
ASTRO_EARTH_NOT_ALLOWED, /**< The Earth cannot be treated as a celestial body seen from an observer on the Earth itself. */
ASTRO_NO_MOON_QUARTER, /**< No lunar quarter occurs inside the specified time range. */
ASTRO_WRONG_MOON_QUARTER, /**< Internal error: Astronomy_NextMoonQuarter found the wrong moon quarter. */
ASTRO_INTERNAL_ERROR, /**< A self-check failed inside the code somewhere, indicating a bug needs to be fixed. */
ASTRO_INVALID_PARAMETER, /**< A parameter value passed to a function was not valid. */
ASTRO_FAIL_APSIS, /**< Special-case logic for finding Neptune/Pluto apsis failed. */
ASTRO_BUFFER_TOO_SMALL, /**< A provided buffer's size is too small to receive the requested data. */
ASTRO_OUT_OF_MEMORY /**< An attempt to allocate memory failed. */
}
astro_status_t;
/**
* @brief A date and time used for astronomical calculations.
*
* This type is of fundamental importance to Astronomy Engine.
* It is used to represent dates and times for all astronomical calculations.
* It is also included in the values returned by many Astronomy Engine functions.
*
* To create a valid astro_time_t value from scratch, call #Astronomy_MakeTime
* (for a given calendar date and time) or #Astronomy_CurrentTime (for the system's
* current date and time).
*
* To adjust an existing astro_time_t by a certain real number of days,
* call #Astronomy_AddDays.
*
* The astro_time_t type contains `ut` to represent Universal Time (UT1/UTC) and
* `tt` to represent Terrestrial Time (TT, also known as *ephemeris time*).
* The difference `tt-ut` is known as *&Delta;T*, and is obtained from
* a model provided by the
* [United States Naval Observatory](http://maia.usno.navy.mil/ser7/).
*
* Both `tt` and `ut` are necessary for performing different astronomical calculations.
* Indeed, certain calculations (such as rise/set times) require both time scales.
* See the documentation for the `ut` and `tt` fields for more detailed information.
*
* In cases where astro_time_t is included in a structure returned by
* a function that can fail, the astro_status_t field `status` will contain a value
* other than `ASTRO_SUCCESS`; in that case the `ut` and `tt` will hold `NAN` (not a number).
* In general, when there is an error code stored in a struct field `status`, the
* caller should ignore all other values in that structure, including the `ut` and `tt`
* inside astro_time_t.
*/
typedef struct
{
/**
* @brief UT1/UTC number of days since noon on January 1, 2000.
*
* The floating point number of days of Universal Time since noon UTC January 1, 2000.
* Astronomy Engine approximates UTC and UT1 as being the same thing, although they are
* not exactly equivalent; UTC and UT1 can disagree by up to &plusmn;0.9 seconds.
* This approximation is sufficient for the accuracy requirements of Astronomy Engine.
*
* Universal Time Coordinate (UTC) is the international standard for legal and civil
* timekeeping and replaces the older Greenwich Mean Time (GMT) standard.
* UTC is kept in sync with unpredictable observed changes in the Earth's rotation
* by occasionally adding leap seconds as needed.
*
* UT1 is an idealized time scale based on observed rotation of the Earth, which
* gradually slows down in an unpredictable way over time, due to tidal drag by the Moon and Sun,
* large scale weather events like hurricanes, and internal seismic and convection effects.
* Conceptually, UT1 drifts from atomic time continuously and erratically, whereas UTC
* is adjusted by a scheduled whole number of leap seconds as needed.
*
* The value in `ut` is appropriate for any calculation involving the Earth's rotation,
* such as calculating rise/set times, culumination, and anything involving apparent
* sidereal time.
*
* Before the era of atomic timekeeping, days based on the Earth's rotation
* were often known as *mean solar days*.
*/
double ut;
/**
* @brief Terrestrial Time days since noon on January 1, 2000.
*
* Terrestrial Time is an atomic time scale defined as a number of days since noon on January 1, 2000.
* In this system, days are not based on Earth rotations, but instead by
* the number of elapsed [SI seconds](https://physics.nist.gov/cuu/Units/second.html)
* divided by 86400. Unlike `ut`, `tt` increases uniformly without adjustments
* for changes in the Earth's rotation.
*
* The value in `tt` is used for calculations of movements not involving the Earth's rotation,
* such as the orbits of planets around the Sun, or the Moon around the Earth.
*
* Historically, Terrestrial Time has also been known by the term *Ephemeris Time* (ET).
*/
double tt;
/**
* @brief For internal use only. Used to optimize Earth tilt calculations.
*/
double psi;
/**
* @brief For internal use only. Used to optimize Earth tilt calculations.
*/
double eps;
}
astro_time_t;
/**
* @brief A calendar date and time expressed in UTC.
*/
typedef struct
{
int year; /**< The year value, e.g. 2019. */
int month; /**< The month value: 1=January, 2=February, ..., 12=December. */
int day; /**< The day of the month in the range 1..31. */
int hour; /**< The hour of the day in the range 0..23. */
int minute; /**< The minute of the hour in the range 0..59. */
double second; /**< The floating point number of seconds in the range [0,60). */
}
astro_utc_t;
/**
* @brief A 3D Cartesian vector whose components are expressed in Astronomical Units (AU).
*/
typedef struct
{
astro_status_t status; /**< `ASTRO_SUCCESS` if this struct is valid; otherwise an error code. */
double x; /**< The Cartesian x-coordinate of the vector in AU. */
double y; /**< The Cartesian y-coordinate of the vector in AU. */
double z; /**< The Cartesian z-coordinate of the vector in AU. */
astro_time_t t; /**< The date and time at which this vector is valid. */
}
astro_vector_t;
/**
* @brief Spherical coordinates: latitude, longitude, distance.
*/
typedef struct
{
astro_status_t status; /**< `ASTRO_SUCCESS` if this struct is valid; otherwise an error code. */
double lat; /**< The latitude angle: -90..+90 degrees. */
double lon; /**< The longitude angle: 0..360 degrees. */
double dist; /**< Distance in AU. */
}
astro_spherical_t;
/**
* @brief An angular value expressed in degrees.
*/
typedef struct
{
astro_status_t status; /**< `ASTRO_SUCCESS` if this struct is valid; otherwise an error code. */
double angle; /**< An angle expressed in degrees. */
}
astro_angle_result_t;
/**
* @brief A celestial body.
*/
typedef enum
{
BODY_INVALID = -1, /**< An invalid or undefined celestial body. */
BODY_MERCURY, /**< Mercury */
BODY_VENUS, /**< Venus */
BODY_EARTH, /**< Earth */
BODY_MARS, /**< Mars */
BODY_JUPITER, /**< Jupiter */
BODY_SATURN, /**< Saturn */
BODY_URANUS, /**< Uranus */
BODY_NEPTUNE, /**< Neptune */
BODY_PLUTO, /**< Pluto */
BODY_SUN, /**< Sun */
BODY_MOON, /**< Moon */
BODY_EMB, /**< Earth/Moon Barycenter */
BODY_SSB /**< Solar System Barycenter */
}
astro_body_t;
#define MIN_BODY BODY_MERCURY /**< Minimum valid astro_body_t value; useful for iteration. */
#define MAX_BODY BODY_SSB /**< Maximum valid astro_body_t value; useful for iteration. */
#define MIN_YEAR 1700 /**< Minimum year value supported by Astronomy Engine. */
#define MAX_YEAR 2200 /**< Maximum year value supported by Astronomy Engine. */
/**
* @brief The location of an observer on (or near) the surface of the Earth.
*
* This structure is passed to functions that calculate phenomena as observed
* from a particular place on the Earth.
*
* You can create this structure directly, or you can call the convenience function
* #Astronomy_MakeObserver# to create one for you.
*/
typedef struct
{
double latitude; /**< Geographic latitude in degrees north (positive) or south (negative) of the equator. */
double longitude; /**< Geographic longitude in degrees east (positive) or west (negative) of the prime meridian at Greenwich, England. */
double height; /**< The height above (positive) or below (negative) sea level, expressed in meters. */
}
astro_observer_t;
/**
* @brief Equatorial angular coordinates.
*
* Coordinates of a celestial body as seen from the Earth (geocentric or topocentric, depending on context),
* oriented with respect to the projection of the Earth's equator onto the sky.
*/
typedef struct
{
astro_status_t status; /**< `ASTRO_SUCCESS` if this struct is valid; otherwise an error code. */
double ra; /**< right ascension in sidereal hours. */
double dec; /**< declination in degrees */
double dist; /**< distance to the celestial body in AU. */
}
astro_equatorial_t;
/**
* @brief Ecliptic angular and Cartesian coordinates.
*
* Coordinates of a celestial body as seen from the center of the Sun (heliocentric),
* oriented with respect to the plane of the Earth's orbit around the Sun (the ecliptic).
*/
typedef struct
{
astro_status_t status; /**< `ASTRO_SUCCESS` if this struct is valid; otherwise an error code. */
double ex; /**< Cartesian x-coordinate: in the direction of the equinox along the ecliptic plane. */
double ey; /**< Cartesian y-coordinate: in the ecliptic plane 90 degrees prograde from the equinox. */
double ez; /**< Cartesian z-coordinate: perpendicular to the ecliptic plane. Positive is north. */
double elat; /**< Latitude in degrees north (positive) or south (negative) of the ecliptic plane. */
double elon; /**< Longitude in degrees around the ecliptic plane prograde from the equinox. */
}
astro_ecliptic_t;
/**
* @brief Coordinates of a celestial body as seen by a topocentric observer.
*
* Contains horizontal and equatorial coordinates seen by an observer on or near
* the surface of the Earth (a topocentric observer).
* Optionally corrected for atmospheric refraction.
*/
typedef struct
{
double azimuth; /**< Compass direction around the horizon in degrees. 0=North, 90=East, 180=South, 270=West. */
double altitude; /**< Angle in degrees above (positive) or below (negative) the observer's horizon. */
double ra; /**< Right ascension in sidereal hours. */
double dec; /**< Declination in degrees. */
}
astro_horizon_t;
/**
* @brief Contains a rotation matrix that can be used to transform one coordinate system to another.
*/
typedef struct
{
astro_status_t status; /**< `ASTRO_SUCCESS` if this struct is valid; otherwise an error code. */
double rot[3][3]; /**< A normalized 3x3 rotation matrix. */
}
astro_rotation_t;
/**
* @brief Selects whether to correct for atmospheric refraction, and if so, how.
*/
typedef enum
{
REFRACTION_NONE, /**< No atmospheric refraction correction (airless). */
REFRACTION_NORMAL, /**< Recommended correction for standard atmospheric refraction. */
REFRACTION_JPLHOR /**< Used only for compatibility testing with JPL Horizons online tool. */
}
astro_refraction_t;
/**
* @brief The result of a search for an astronomical event.
*/
typedef struct
{
astro_status_t status; /**< `ASTRO_SUCCESS` if this struct is valid; otherwise an error code. */
astro_time_t time; /**< The time at which a searched-for event occurs. */
}
astro_search_result_t;
/**
* @brief
* The dates and times of changes of season for a given calendar year.
* Call #Astronomy_Seasons to calculate this data structure for a given year.
*/
typedef struct
{
astro_status_t status; /**< `ASTRO_SUCCESS` if this struct is valid; otherwise an error code. */
astro_time_t mar_equinox; /**< The date and time of the March equinox for the specified year. */
astro_time_t jun_solstice; /**< The date and time of the June soltice for the specified year. */
astro_time_t sep_equinox; /**< The date and time of the September equinox for the specified year. */
astro_time_t dec_solstice; /**< The date and time of the December solstice for the specified year. */
}
astro_seasons_t;
/**
* @brief A lunar quarter event (new moon, first quarter, full moon, or third quarter) along with its date and time.
*/
typedef struct
{
astro_status_t status; /**< `ASTRO_SUCCESS` if this struct is valid; otherwise an error code. */
int quarter; /**< 0=new moon, 1=first quarter, 2=full moon, 3=third quarter. */
astro_time_t time; /**< The date and time of the lunar quarter. */
}
astro_moon_quarter_t;
/**
* @brief A real value returned by a function whose ascending root is to be found.
*
* When calling #Astronomy_Search, the caller must pass in a callback function
* compatible with the function-pointer type #astro_search_func_t
* whose ascending root is to be found. That callback function must return astro_func_result_t.
* If the function call is successful, it will set `status` to `ASTRO_SUCCESS` and `value`
* to the numeric value appropriate for the given date and time.
* If the call fails for some reason, it should set `status` to an appropriate error value
* other than `ASTRO_SUCCESS`; in the error case, to guard against any possible misuse of `value`,
* it is recommended to set `value` to `NAN`, though this is not strictly necessary.
*/
typedef struct
{
astro_status_t status; /**< `ASTRO_SUCCESS` if this struct is valid; otherwise an error code. */
double value; /**< The value returned by a function whose ascending root is to be found. */
}
astro_func_result_t;
/**
* @brief A pointer to a function that is to be passed as a callback to #Astronomy_Search.
*
* The function #Astronomy_Search numerically solves for the time that a given event occurs.
* An event is defined as the time when an arbitrary function transitions between having
* a negative value and a non-negative value. This transition is called an *ascending root*.
*
* The type astro_search_func_t represents such a callback function that accepts a
* custom `context` pointer and an astro_time_t representing the time to probe.
* The function returns an astro_func_result_t that contains either a real
* number in `value` or an error code in `status` that aborts the search.
*
* The `context` points to some data whose type varies depending on the callback function.
* It can contain any auxiliary parameters (other than time) needed to evaluate the function.
* For example, a function may pertain to a specific celestial body, in which case `context`
* may point to a value of type astro_body_t. The `context` parameter is supplied by
* the caller of #Astronomy_Search, which passes it along to every call to the callback function.
* If the caller of `Astronomy_Search` knows that the callback function does not need a context,
* it is safe to pass `NULL` as the context pointer.
*/
typedef astro_func_result_t (* astro_search_func_t) (void *context, astro_time_t time);
/**
* @brief A pointer to a function that calculates Delta T.
*
* Delta T is the discrepancy between times measured using an atomic clock
* and times based on observations of the Earth's rotation, which is gradually
* slowing down over time. Delta T = TT - UT, where
* TT = Terrestrial Time, based on atomic time, and
* UT = Universal Time, civil time based on the Earth's rotation.
* Astronomy Engine defaults to using a Delta T function defined by
* Espenak and Meeus in their "Five Millennium Canon of Solar Eclipses".
* See: https://eclipse.gsfc.nasa.gov/SEhelp/deltatpoly2004.html
*/
typedef double (* astro_deltat_func) (double ut);
double Astronomy_DeltaT_EspenakMeeus(double ut);
double Astronomy_DeltaT_JplHorizons(double ut);
void Astronomy_SetDeltaTFunction(astro_deltat_func func);
/**
* @brief Indicates whether a body (especially Mercury or Venus) is best seen in the morning or evening.
*/
typedef enum
{
VISIBLE_MORNING, /**< The body is best visible in the morning, before sunrise. */
VISIBLE_EVENING /**< The body is best visible in the evening, after sunset. */
}
astro_visibility_t;
/**
* @brief
* Contains information about the visibility of a celestial body at a given date and time.
* See #Astronomy_Elongation for more detailed information about the members of this structure.
* See also #Astronomy_SearchMaxElongation for how to search for maximum elongation events.
*/
typedef struct
{
astro_status_t status; /**< `ASTRO_SUCCESS` if this struct is valid; otherwise an error code. */
astro_time_t time; /**< The date and time of the observation. */
astro_visibility_t visibility; /**< Whether the body is best seen in the morning or the evening. */
double elongation; /**< The angle in degrees between the body and the Sun, as seen from the Earth. */
double ecliptic_separation; /**< The difference between the ecliptic longitudes of the body and the Sun, as seen from the Earth. */
}
astro_elongation_t;
/**
* @brief Information about a celestial body crossing a specific hour angle.
*
* Returned by the function #Astronomy_SearchHourAngle to report information about
* a celestial body crossing a certain hour angle as seen by a specified topocentric observer.
*/
typedef struct
{
astro_status_t status; /**< `ASTRO_SUCCESS` if this struct is valid; otherwise an error code. */
astro_time_t time; /**< The date and time when the body crosses the specified hour angle. */
astro_horizon_t hor; /**< Apparent coordinates of the body at the time it crosses the specified hour angle. */
}
astro_hour_angle_t;
/**
* @brief Information about the brightness and illuminated shape of a celestial body.
*
* Returned by the functions #Astronomy_Illumination and #Astronomy_SearchPeakMagnitude
* to report the visual magnitude and illuminated fraction of a celestial body at a given date and time.
*/
typedef struct
{
astro_status_t status; /**< `ASTRO_SUCCESS` if this struct is valid; otherwise an error code. */
astro_time_t time; /**< The date and time of the observation. */
double mag; /**< The visual magnitude of the body. Smaller values are brighter. */
double phase_angle; /**< The angle in degrees between the Sun and the Earth, as seen from the body. Indicates the body's phase as seen from the Earth. */
double helio_dist; /**< The distance between the Sun and the body at the observation time. */
double ring_tilt; /**< For Saturn, the tilt angle in degrees of its rings as seen from Earth. For all other bodies, 0. */
}
astro_illum_t;
/**
* @brief The type of apsis: pericenter (closest approach) or apocenter (farthest distance).
*/
typedef enum
{
APSIS_PERICENTER, /**< The body is at its closest approach to the object it orbits. */
APSIS_APOCENTER, /**< The body is at its farthest distance from the object it orbits. */
APSIS_INVALID /**< Undefined or invalid apsis. */
}
astro_apsis_kind_t;
/**
* @brief An apsis event: pericenter (closest approach) or apocenter (farthest distance).
*
* For the Moon orbiting the Earth, or a planet orbiting the Sun, an *apsis* is an
* event where the orbiting body reaches its closest or farthest point from the primary body.
* The closest approach is called *pericenter* and the farthest point is *apocenter*.
*
* More specific terminology is common for particular orbiting bodies.
* The Moon's closest approach to the Earth is called *perigee* and its farthest
* point is called *apogee*. The closest approach of a planet to the Sun is called
* *perihelion* and the furthest point is called *aphelion*.
*
* This data structure is returned by #Astronomy_SearchLunarApsis and #Astronomy_NextLunarApsis
* to iterate through consecutive alternating perigees and apogees.
*/
typedef struct
{
astro_status_t status; /**< `ASTRO_SUCCESS` if this struct is valid; otherwise an error code. */
astro_time_t time; /**< The date and time of the apsis. */
astro_apsis_kind_t kind; /**< Whether this is a pericenter or apocenter event. */
double dist_au; /**< The distance between the centers of the bodies in astronomical units. */
double dist_km; /**< The distance between the centers of the bodies in kilometers. */
}
astro_apsis_t;
/**
* @brief The different kinds of lunar/solar eclipses.
*/
typedef enum
{
ECLIPSE_NONE, /**< No eclipse found. */
ECLIPSE_PENUMBRAL, /**< A penumbral lunar eclipse. (Never used for a solar eclipse.) */
ECLIPSE_PARTIAL, /**< A partial lunar/solar eclipse. */
ECLIPSE_ANNULAR, /**< An annular solar eclipse. (Never used for a lunar eclipse.) */
ECLIPSE_TOTAL /**< A total lunar/solar eclipse. */
}
astro_eclipse_kind_t;
/**
* @brief Information about a lunar eclipse.
*
* Returned by #Astronomy_SearchLunarEclipse or #Astronomy_NextLunarEclipse
* to report information about a lunar eclipse event.
* If a lunar eclipse is found, `status` holds `ASTRO_SUCCESS` and the other fields are set.
* If `status` holds any other value, it is an error code and the other fields are undefined.
*
* When a lunar eclipse is found, it is classified as penumbral, partial, or total.
* Penumbral eclipses are difficult to observe, because the moon is only slightly dimmed
* by the Earth's penumbra; no part of the Moon touches the Earth's umbra.
* Partial eclipses occur when part, but not all, of the Moon touches the Earth's umbra.
* Total eclipses occur when the entire Moon passes into the Earth's umbra.
*
* The `kind` field thus holds `ECLIPSE_PENUMBRAL`, `ECLIPSE_PARTIAL`, or `ECLIPSE_TOTAL`,
* depending on the kind of lunar eclipse found.
*
* Field `peak` holds the date and time of the center of the eclipse, when it is at its peak.
*
* Fields `sd_penum`, `sd_partial`, and `sd_total` hold the semi-duration of each phase
* of the eclipse, which is half of the amount of time the eclipse spends in each
* phase (expressed in minutes), or 0 if the eclipse never reaches that phase.
* By converting from minutes to days, and subtracting/adding with `center`, the caller
* may determine the date and time of the beginning/end of each eclipse phase.
*/
typedef struct
{
astro_status_t status; /**< `ASTRO_SUCCESS` if this struct is valid; otherwise an error code. */
astro_eclipse_kind_t kind; /**< The type of lunar eclipse found. */
astro_time_t peak; /**< The time of the eclipse at its peak. */
double sd_penum; /**< The semi-duration of the penumbral phase in minutes. */
double sd_partial; /**< The semi-duration of the partial phase in minutes, or 0.0 if none. */
double sd_total; /**< The semi-duration of the total phase in minutes, or 0.0 if none. */
}
astro_lunar_eclipse_t;
/**
* @brief Reports the time and geographic location of the peak of a solar eclipse.
*
* Returned by #Astronomy_SearchGlobalSolarEclipse or #Astronomy_NextGlobalSolarEclipse
* to report information about a solar eclipse event.
* If a solar eclipse is found, `status` holds `ASTRO_SUCCESS` and `kind`, `peak`, and `distance`
* have valid values. The `latitude` and `longitude` are set only for total and annular eclipses
* (see more below).
* If `status` holds any value other than `ASTRO_SUCCESS`, it is an error code;
* in that case, `kind` holds `ECLIPSE_NONE` and all the other fields are undefined.
*
* Field `peak` holds the date and time of the peak of the eclipse, defined as
* the instant when the axis of the Moon's shadow cone passes closest to the Earth's center.
*
* The eclipse is classified as partial, annular, or total, depending on the
* maximum amount of the Sun's disc obscured, as seen at the peak location
* on the surface of the Earth.
*
* The `kind` field thus holds `ECLIPSE_PARTIAL`, `ECLIPSE_ANNULAR`, or `ECLIPSE_TOTAL`.
* A total eclipse is when the peak observer sees the Sun completely blocked by the Moon.
* An annular eclipse is like a total eclipse, but the Moon is too far from the Earth's surface
* to completely block the Sun; instead, the Sun takes on a ring-shaped appearance.
* A partial eclipse is when the Moon blocks part of the Sun's disc, but nobody on the Earth
* observes either a total or annular eclipse.
*
* If `kind` is `ECLIPSE_TOTAL` or `ECLIPSE_ANNULAR`, the `latitude` and `longitude`
* fields give the geographic coordinates of the center of the Moon's shadow projected
* onto the daytime side of the Earth at the instant of the eclipse's peak.
* If `kind` has any other value, `latitude` and `longitude` are undefined and should
* not be used.
*/
typedef struct
{
astro_status_t status; /**< `ASTRO_SUCCESS` if this struct is valid; otherwise an error code. */
astro_eclipse_kind_t kind; /**< The type of solar eclipse found. */
astro_time_t peak; /**< The date and time of the eclipse at its peak. */
double distance; /**< The distance between the Sun/Moon shadow axis and the center of the Earth, in kilometers. */
double latitude; /**< The geographic latitude at the center of the peak eclipse shadow. */
double longitude; /**< The geographic longitude at the center of the peak eclipse shadow. */
}
astro_global_solar_eclipse_t;
/**
* @brief Holds a time and the observed altitude of the Sun at that time.
*
* When reporting a solar eclipse observed at a specific location on the Earth
* (a "local" solar eclipse), a series of events occur. In addition
* to the time of each event, it is important to know the altitude of the Sun,
* because each event may be invisible to the observer if the Sun is below
* the horizon (i.e. it at night).
*
* If `altitude` is negative, the event is theoretical only; it would be
* visible if the Earth were transparent, but the observer cannot actually see it.
* If `altitude` is positive but less than a few degrees, visibility will be impaired by
* atmospheric interference (sunrise or sunset conditions).
*/
typedef struct
{
astro_time_t time; /**< The date and time of the event. */
double altitude; /**< The angular altitude of the center of the Sun above/below the horizon, at `time`, corrected for atmospheric refraction and expressed in degrees. */
}
astro_eclipse_event_t;
/**
* @brief Information about a solar eclipse as seen by an observer at a given time and geographic location.
*
* Returned by #Astronomy_SearchLocalSolarEclipse or #Astronomy_NextLocalSolarEclipse
* to report information about a solar eclipse as seen at a given geographic location.
* If a solar eclipse is found, `status` holds `ASTRO_SUCCESS` and the other fields are set.
* If `status` holds any other value, it is an error code and the other fields are undefined.
*
* When a solar eclipse is found, it is classified as partial, annular, or total.
* The `kind` field thus holds `ECLIPSE_PARTIAL`, `ECLIPSE_ANNULAR`, or `ECLIPSE_TOTAL`.
* A partial solar eclipse is when the Moon does not line up directly enough with the Sun
* to completely block the Sun's light from reaching the observer.
* An annular eclipse occurs when the Moon's disc is completely visible against the Sun
* but the Moon is too far away to completely block the Sun's light; this leaves the
* Sun with a ring-like appearance.
* A total eclipse occurs when the Moon is close enough to the Earth and aligned with the
* Sun just right to completely block all sunlight from reaching the observer.
*
* There are 5 "event" fields, each of which contains a time and a solar altitude.
* Field `peak` holds the date and time of the center of the eclipse, when it is at its peak.
* The fields `partial_begin` and `partial_end` are always set, and indicate when
* the eclipse begins/ends. If the eclipse reaches totality or becomes annular,
* `total_begin` and `total_end` indicate when the total/annular phase begins/ends.
* When an event field is valid, the caller must also check its `altitude` field to
* see whether the Sun is above the horizon at that time. See #astro_eclipse_kind_t
* for more information.
*/
typedef struct
{
astro_status_t status; /**< `ASTRO_SUCCESS` if this struct is valid; otherwise an error code. */
astro_eclipse_kind_t kind; /**< The type of solar eclipse found: `ECLIPSE_PARTIAL`, `ECLIPSE_ANNULAR`, or `ECLIPSE_TOTAL`. */
astro_eclipse_event_t partial_begin; /**< The time and Sun altitude at the beginning of the eclipse. */
astro_eclipse_event_t total_begin; /**< If this is an annular or a total eclipse, the time and Sun altitude when annular/total phase begins; otherwise invalid. */
astro_eclipse_event_t peak; /**< The time and Sun altitude when the eclipse reaches its peak. */
astro_eclipse_event_t total_end; /**< If this is an annular or a total eclipse, the time and Sun altitude when annular/total phase ends; otherwise invalid. */
astro_eclipse_event_t partial_end; /**< The time and Sun altitude at the end of the eclipse. */
}
astro_local_solar_eclipse_t;
/**
* @brief Information about a transit of Mercury or Venus, as seen from the Earth.
*
* Returned by #Astronomy_SearchTransit or #Astronomy_NextTransit to report
* information about a transit of Mercury or Venus.
* A transit is when Mercury or Venus passes between the Sun and Earth so that
* the other planet is seen in silhouette against the Sun.
*
* The `start` field reports the moment in time when the planet first becomes
* visible against the Sun in its background.
* The `peak` field reports when the planet is most aligned with the Sun,
* as seen from the Earth.
* The `finish` field reports the last moment when the planet is visible
* against the Sun in its background.
*
* The calculations are performed from the point of view of a geocentric observer.
*/
typedef struct
{
astro_status_t status; /**< `ASTRO_SUCCESS` if this struct is valid; otherwise an error code. */
astro_time_t start; /**< Date and time at the beginning of the transit. */
astro_time_t peak; /**< Date and time of the peak of the transit. */
astro_time_t finish; /**< Date and time at the end of the transit. */
double separation; /**< Angular separation in arcminutes between the centers of the Sun and the planet at time `peak`. */
}
astro_transit_t;
/**
* @brief Aberration calculation options.
*
* [Aberration](https://en.wikipedia.org/wiki/Aberration_of_light) is an effect
* causing the apparent direction of an observed body to be shifted due to transverse
* movement of the Earth with respect to the rays of light coming from that body.
* This angular correction can be anywhere from 0 to about 20 arcseconds,
* depending on the position of the observed body relative to the instantaneous
* velocity vector of the Earth.
*
* Some Astronomy Engine functions allow optional correction for aberration by
* passing in a value of this enumerated type.
*
* Aberration correction is useful to improve accuracy of coordinates of
* apparent locations of bodies seen from the Earth.
* However, because aberration affects not only the observed body (such as a planet)
* but the surrounding stars, aberration may be unhelpful (for example)
* for determining exactly when a planet crosses from one constellation to another.
*/
typedef enum
{
ABERRATION, /**< Request correction for aberration. */
NO_ABERRATION /**< Do not correct for aberration. */
}
astro_aberration_t;
/**
* @brief Selects the date for which the Earth's equator is to be used for representing equatorial coordinates.
*
* The Earth's equator is not always in the same plane due to precession and nutation.
*
* Sometimes it is useful to have a fixed plane of reference for equatorial coordinates
* across different calendar dates. In these cases, a fixed *epoch*, or reference time,
* is helpful. Astronomy Engine provides the J2000 epoch for such cases. This refers
* to the plane of the Earth's orbit as it was on noon UTC on 1 January 2000.
*
* For some other purposes, it is more helpful to represent coordinates using the Earth's
* equator exactly as it is on that date. For example, when calculating rise/set times
* or horizontal coordinates, it is most accurate to use the orientation of the Earth's
* equator at that same date and time. For these uses, Astronomy Engine allows *of-date*
* calculations.
*/
typedef enum
{
EQUATOR_J2000, /**< Represent equatorial coordinates in the J2000 epoch. */
EQUATOR_OF_DATE /**< Represent equatorial coordinates using the Earth's equator at the given date and time. */
}
astro_equator_date_t;
/**
* @brief Selects whether to search for a rise time or a set time.
*
* The #Astronomy_SearchRiseSet function finds the rise or set time of a body
* depending on the value of its `direction` parameter.
*/
typedef enum
{
DIRECTION_RISE = +1, /**< Search for the time a body begins to rise above the horizon. */
DIRECTION_SET = -1, /**< Search for the time a body finishes sinking below the horizon. */
}
astro_direction_t;
/**
* @brief Reports the constellation that a given celestial point lies within.
*
* The #Astronomy_Constellation function returns this struct
* to report which constellation corresponds with a given point in the sky.
* Constellations are defined with respect to the B1875 equatorial system
* per IAU standard. Although `Astronomy.Constellation` requires J2000 equatorial
* coordinates, the struct contains converted B1875 coordinates for reference.
*/
typedef struct
{
astro_status_t status; /**< `ASTRO_SUCCESS` if this struct is valid; otherwise an error code. */
const char *symbol; /**< 3-character mnemonic symbol for the constellation, e.g. "Ori". */
const char *name; /**< Full name of constellation, e.g. "Orion". */
double ra_1875; /**< Right ascension expressed in B1875 coordinates. */
double dec_1875; /**< Declination expressed in B1875 coordinates. */
}
astro_constellation_t;
/**
* @brief Selects the output format of the function #Astronomy_FormatTime.
*/
typedef enum
{
TIME_FORMAT_DAY, /**< Truncate to UTC calendar date only, e.g. `2020-12-31`. Buffer size must be at least 11 characters. */
TIME_FORMAT_MINUTE, /**< Round to nearest UTC minute, e.g. `2020-12-31T15:47Z`. Buffer size must be at least 18 characters. */
TIME_FORMAT_SECOND, /**< Round to nearest UTC second, e.g. `2020-12-31T15:47:32Z`. Buffer size must be at least 21 characters. */
TIME_FORMAT_MILLI /**< Round to nearest UTC millisecond, e.g. `2020-12-31T15:47:32.397Z`. Buffer size must be at least 25 characters. */
}
astro_time_format_t;
#define TIME_TEXT_BYTES 25 /**< The smallest number of characters that is always large enough for #Astronomy_FormatTime. */
/*---------- functions ----------*/
void Astronomy_Reset(void);
double Astronomy_VectorLength(astro_vector_t vector);
const char *Astronomy_BodyName(astro_body_t body);
astro_body_t Astronomy_BodyCode(const char *name);
astro_observer_t Astronomy_MakeObserver(double latitude, double longitude, double height);
astro_time_t Astronomy_CurrentTime(void);
astro_time_t Astronomy_MakeTime(int year, int month, int day, int hour, int minute, double second);
astro_time_t Astronomy_TimeFromUtc(astro_utc_t utc);
astro_utc_t Astronomy_UtcFromTime(astro_time_t time);
astro_status_t Astronomy_FormatTime(astro_time_t time, astro_time_format_t format, char *text, size_t size);
astro_time_t Astronomy_TimeFromDays(double ut);
astro_time_t Astronomy_AddDays(astro_time_t time, double days);
astro_func_result_t Astronomy_HelioDistance(astro_body_t body, astro_time_t time);
astro_vector_t Astronomy_HelioVector(astro_body_t body, astro_time_t time);
astro_vector_t Astronomy_GeoVector(astro_body_t body, astro_time_t time, astro_aberration_t aberration);
astro_vector_t Astronomy_GeoMoon(astro_time_t time);
astro_equatorial_t Astronomy_Equator(
astro_body_t body,
astro_time_t *time,
astro_observer_t observer,
astro_equator_date_t equdate,
astro_aberration_t aberration
);
astro_ecliptic_t Astronomy_SunPosition(astro_time_t time);
astro_ecliptic_t Astronomy_Ecliptic(astro_vector_t equ);
astro_angle_result_t Astronomy_EclipticLongitude(astro_body_t body, astro_time_t time);
astro_horizon_t Astronomy_Horizon(
astro_time_t *time,
astro_observer_t observer,
double ra,
double dec,
astro_refraction_t refraction);
astro_angle_result_t Astronomy_AngleFromSun(astro_body_t body, astro_time_t time);
astro_elongation_t Astronomy_Elongation(astro_body_t body, astro_time_t time);
astro_elongation_t Astronomy_SearchMaxElongation(astro_body_t body, astro_time_t startTime);
astro_angle_result_t Astronomy_LongitudeFromSun(astro_body_t body, astro_time_t time);
astro_search_result_t Astronomy_SearchRelativeLongitude(astro_body_t body, double targetRelLon, astro_time_t startTime);
astro_angle_result_t Astronomy_MoonPhase(astro_time_t time);
astro_search_result_t Astronomy_SearchMoonPhase(double targetLon, astro_time_t startTime, double limitDays);
astro_moon_quarter_t Astronomy_SearchMoonQuarter(astro_time_t startTime);
astro_moon_quarter_t Astronomy_NextMoonQuarter(astro_moon_quarter_t mq);
astro_lunar_eclipse_t Astronomy_SearchLunarEclipse(astro_time_t startTime);
astro_lunar_eclipse_t Astronomy_NextLunarEclipse(astro_time_t prevEclipseTime);
astro_global_solar_eclipse_t Astronomy_SearchGlobalSolarEclipse(astro_time_t startTime);
astro_global_solar_eclipse_t Astronomy_NextGlobalSolarEclipse(astro_time_t prevEclipseTime);
astro_local_solar_eclipse_t Astronomy_SearchLocalSolarEclipse(astro_time_t startTime, astro_observer_t observer);
astro_local_solar_eclipse_t Astronomy_NextLocalSolarEclipse(astro_time_t prevEclipseTime, astro_observer_t observer);
astro_transit_t Astronomy_SearchTransit(astro_body_t body, astro_time_t startTime);
astro_transit_t Astronomy_NextTransit(astro_body_t body, astro_time_t prevTransitTime);
astro_search_result_t Astronomy_Search(
astro_search_func_t func,
void *context,
astro_time_t t1,
astro_time_t t2,
double dt_tolerance_seconds);
astro_search_result_t Astronomy_SearchSunLongitude(
double targetLon,
astro_time_t startTime,
double limitDays);
astro_hour_angle_t Astronomy_SearchHourAngle(
astro_body_t body,
astro_observer_t observer,
double hourAngle,
astro_time_t startTime);
astro_search_result_t Astronomy_SearchRiseSet(
astro_body_t body,
astro_observer_t observer,
astro_direction_t direction,
astro_time_t startTime,
double limitDays);
astro_seasons_t Astronomy_Seasons(int year);
astro_illum_t Astronomy_Illumination(astro_body_t body, astro_time_t time);
astro_illum_t Astronomy_SearchPeakMagnitude(astro_body_t body, astro_time_t startTime);
astro_apsis_t Astronomy_SearchLunarApsis(astro_time_t startTime);
astro_apsis_t Astronomy_NextLunarApsis(astro_apsis_t apsis);
astro_apsis_t Astronomy_SearchPlanetApsis(astro_body_t body, astro_time_t startTime);
astro_apsis_t Astronomy_NextPlanetApsis(astro_body_t body, astro_apsis_t apsis);
astro_rotation_t Astronomy_InverseRotation(astro_rotation_t rotation);
astro_rotation_t Astronomy_CombineRotation(astro_rotation_t a, astro_rotation_t b);
astro_vector_t Astronomy_VectorFromSphere(astro_spherical_t sphere, astro_time_t time);
astro_spherical_t Astronomy_SphereFromVector(astro_vector_t vector);
astro_vector_t Astronomy_VectorFromEquator(astro_equatorial_t equ, astro_time_t time);
astro_equatorial_t Astronomy_EquatorFromVector(astro_vector_t vector);
astro_vector_t Astronomy_VectorFromHorizon(astro_spherical_t sphere, astro_time_t time, astro_refraction_t refraction);
astro_spherical_t Astronomy_HorizonFromVector(astro_vector_t vector, astro_refraction_t refraction);
astro_vector_t Astronomy_RotateVector(astro_rotation_t rotation, astro_vector_t vector);
astro_rotation_t Astronomy_Rotation_EQD_EQJ(astro_time_t time);
astro_rotation_t Astronomy_Rotation_EQD_ECL(astro_time_t time);
astro_rotation_t Astronomy_Rotation_EQD_HOR(astro_time_t time, astro_observer_t observer);
astro_rotation_t Astronomy_Rotation_EQJ_EQD(astro_time_t time);
astro_rotation_t Astronomy_Rotation_EQJ_ECL(void);
astro_rotation_t Astronomy_Rotation_EQJ_HOR(astro_time_t time, astro_observer_t observer);
astro_rotation_t Astronomy_Rotation_ECL_EQD(astro_time_t time);
astro_rotation_t Astronomy_Rotation_ECL_EQJ(void);
astro_rotation_t Astronomy_Rotation_ECL_HOR(astro_time_t time, astro_observer_t observer);
astro_rotation_t Astronomy_Rotation_HOR_EQD(astro_time_t time, astro_observer_t observer);
astro_rotation_t Astronomy_Rotation_HOR_EQJ(astro_time_t time, astro_observer_t observer);
astro_rotation_t Astronomy_Rotation_HOR_ECL(astro_time_t time, astro_observer_t observer);
double Astronomy_Refraction(astro_refraction_t refraction, double altitude);
double Astronomy_InverseRefraction(astro_refraction_t refraction, double bent_altitude);
astro_constellation_t Astronomy_Constellation(double ra, double dec);
#ifdef __cplusplus
}
#endif
#endif /* ifndef __ASTRONOMY_H */