#include <stdint.h>
#include <math.h>
#include <time.h>
#include <stdio.h>
#include "earth.h"
#include "lunsol.h"

Include dependency graph for orbit.h:

This graph shows which files directly or indirectly include this file:

Classes
struct	ATTITUDE

struct	BROUWER

struct	GEODETIC

struct	KEPLER

struct	NUTATION

struct	PRECESSION

struct	RADEC

struct	SGP4

struct	TLE_VALUES

struct	TOPOCENTRIC

Macros
#define	DPI 3.14159265358979323846

#define	D2PI 6.28318530717958647692

#define	D3PI 9.42477796076937971538

#define	FP_ERRVAL -1.0e-20 /* Error value from f.p. routines */

#define	DTOR(X) ((X) * DPI/180.0)

#define	RTOD(X) ((X) * 180.0/DPI)

#define	AN2PI(X) fmod(fmod((X), D2PI) + D2PI, D2PI)

#define	ANPI(X) (fmod(fmod((X), D2PI) + D3PI, D2PI) - DPI)

#define	AN360(X) fmod(fmod((X), 360.0) + 360.0, 360.0)

#define	ASTOR(X) ((X) * DPI/(180.0 * 3600.0))

#define	ASPCTORPD(X) ((X) * DPI/(180.0 * 3600.0 * 36525.0))

#define	J2000 (51545.0)

Functions
int	blinit (struct BROUWER bp, char *errstr)

int	blosc (struct BROUWER bp, double delt, struct KEPLER kp, char **errstr)

void	ctogd (double r[3], double gha, struct GEODETIC *geod, double dgeod[3][3])

int	ctok (double r[6], struct KEPLER keplr, char *errmsg)

void	ctotc (double r[3], struct GEODETIC obs, double gha, struct TOPOCENTRIC top, double daer[3][3])

double	eanom (double manom, double ecc, char **errstr)

int	efitoeci (double r[6], double gha, double rp[6])

int	efrtoeci (double r[6], double gha, double rp[6])

int	ecitoefi (double r[6], double gha, double rp[6])

int	ecitoefr (double r[6], double gha, double rp[6])

double	gmha (double tjd)

double	gmhadot (double tjd)

void	caldat (int32_t julian, int year, int month, int *day)

double	itojul (int32_t date, int32_t time)

int32_t	julday (int year, int month, int day)

void	jultoi (double tjd, int32_t date, int32_t time)

void	jultotm (double tjd, struct tm *time)

double	tmtojul (struct tm *time)

int	ktoc (struct KEPLER kp, double r[6], char *errstr)

int	ktosgp4 (struct KEPLER kepler, struct SGP4 sgp4, char **errmsg)

int	locate (double r[6], struct ATTITUDE sat, struct ATTITUDE scanner, double loc[3])

void	moonpos (double tjd, double r[3])

void	nut_angles (double tjd, struct NUTATION angles, struct NUTATION rates)

void	nut_matrix (double tjd, double a[3][3])

void	obliq (double tjd, double mood, double dmood)

void	pre_angles (double tjd0, double tjd1, struct PRECESSION *angles)

void	pre_reduce (double tjd0, struct RADEC rad0, double tjd1, struct RADEC rad1)

void	rdtotc (struct RADEC rad, struct GEODETIC obs, double gmha, struct TOPOCENTRIC *top)

double	refract (double alt, double temp, double pressure)

double	unrefract (double alt, double temp, double pressure)

int	sgp4_init (struct SGP4 sgp4, char *errstr)

int	sgp4_pred (struct SGP4 sgp4, double tsince, double rect[6], char *errstr)

double	sgp4_orbit (struct SGP4 sgp4, struct TLE_VALUES tv, double tsince)

int	sgp4_tle (double epoch, struct SGP4 sgp4, char line1, char line2, char **errstr)

int	sunpos (double tjd, double r[3], char **errstr)

double	tconv (double tjd, char conv[], char **errstr)

int	tcset (double x, char what[], char **errstr)

int	tle_parse (char line1, char line2, struct TLE_VALUES tv, char *errstr)

Macro Definition Documentation

◆ AN2PI

#define AN2PI ( X ) fmod(fmod((X), D2PI) + D2PI, D2PI)

Definition at line 57 of file orbit.h.

◆ AN360

#define AN360 ( X ) fmod(fmod((X), 360.0) + 360.0, 360.0)

Definition at line 63 of file orbit.h.

◆ ANPI

#define ANPI ( X ) (fmod(fmod((X), D2PI) + D3PI, D2PI) - DPI)

Definition at line 60 of file orbit.h.

◆ ASPCTORPD

#define ASPCTORPD ( X ) ((X) * DPI/(180.0 * 3600.0 * 36525.0))

Definition at line 69 of file orbit.h.

◆ ASTOR

#define ASTOR ( X ) ((X) * DPI/(180.0 * 3600.0))

Definition at line 66 of file orbit.h.

◆ D2PI

#define D2PI 6.28318530717958647692

Definition at line 45 of file orbit.h.

◆ D3PI

#define D3PI 9.42477796076937971538

Definition at line 46 of file orbit.h.

◆ DPI

#define DPI 3.14159265358979323846

Definition at line 44 of file orbit.h.

◆ DTOR

#define DTOR ( X ) ((X) * DPI/180.0)

Definition at line 51 of file orbit.h.

◆ FP_ERRVAL

#define FP_ERRVAL -1.0e-20 /* Error value from f.p. routines */

Definition at line 48 of file orbit.h.

◆ J2000

#define J2000 (51545.0)

Definition at line 72 of file orbit.h.

◆ RTOD

#define RTOD ( X ) ((X) * 180.0/DPI)

Definition at line 54 of file orbit.h.

Function Documentation

◆ blinit()

int blinit	(	struct BROUWER *	bp,
		char **	errstr
	)

◆ blosc()

int blosc	(	struct BROUWER *	bp,
		double	delt,
		struct KEPLER *	kp,
		char **	errstr
	)

◆ caldat()

void caldat	(	int32_t	julian,
		int *	year,
		int *	month,
		int *	day
	)

Definition at line 75 of file julian.c.

◆ ctogd()

void ctogd	(	double	r[3],
		double	gha,
		struct GEODETIC *	geod,
		double	dgeod[3][3]
	)

◆ ctok()

int ctok	(	double	r[6],
		struct KEPLER *	keplr,
		char **	errmsg
	)

◆ ctotc()

void ctotc	(	double	r[3],
		struct GEODETIC *	obs,
		double	gha,
		struct TOPOCENTRIC *	top,
		double	daer[3][3]
	)

◆ eanom()

double eanom	(	double	manom,
		double	ecc,
		char **	errstr
	)

Definition at line 53 of file eanom.c.

◆ ecitoefi()

int ecitoefi	(	double	r[6],
		double	gha,
		double	rp[6]
	)

◆ ecitoefr()

int ecitoefr	(	double	r[6],
		double	gha,
		double	rp[6]
	)

◆ efitoeci()

int efitoeci	(	double	r[6],
		double	gha,
		double	rp[6]
	)

◆ efrtoeci()

int efrtoeci	(	double	r[6],
		double	gha,
		double	rp[6]
	)

◆ gmha()

double gmha ( double tjd )

Definition at line 61 of file gmha.c.

◆ gmhadot()

double gmhadot ( double tjd )

Definition at line 78 of file gmha.c.

◆ itojul()

double itojul	(	int32_t	date,
		int32_t	time
	)

Definition at line 100 of file time-utils.c.

◆ julday()

int32_t julday	(	int	year,
		int	month,
		int	day
	)

Definition at line 37 of file julian.c.

◆ jultoi()

void jultoi	(	double	tjd,
		int32_t *	date,
		int32_t *	time
	)

Definition at line 134 of file time-utils.c.

◆ jultotm()

void jultotm	(	double	tjd,
		struct tm *	time
	)

Definition at line 62 of file time-utils.c.

◆ ktoc()

int ktoc	(	struct KEPLER *	kp,
		double	r[6],
		char **	errstr
	)

◆ ktosgp4()

int ktosgp4	(	struct KEPLER *	kepler,
		struct SGP4 *	sgp4,
		char **	errmsg
	)

◆ locate()

int locate	(	double	r[6],
		struct ATTITUDE *	sat,
		struct ATTITUDE *	scanner,
		double	loc[3]
	)

◆ moonpos()

void moonpos	(	double	tjd,
		double	r[3]
	)

◆ nut_angles()

void nut_angles	(	double	tjd,
		struct NUTATION *	angles,
		struct NUTATION *	rates
	)

◆ nut_matrix()

void nut_matrix	(	double	tjd,
		double	a[3][3]
	)

◆ obliq()

void obliq	(	double	tjd,
		double *	mood,
		double *	dmood
	)

Definition at line 35 of file obliq.c.

◆ pre_angles()

void pre_angles	(	double	tjd0,
		double	tjd1,
		struct PRECESSION *	angles
	)

◆ pre_reduce()

void pre_reduce	(	double	tjd0,
		struct RADEC *	rad0,
		double	tjd1,
		struct RADEC *	rad1
	)

◆ rdtotc()

void rdtotc	(	struct RADEC *	rad,
		struct GEODETIC *	obs,
		double	gmha,
		struct TOPOCENTRIC *	top
	)

◆ refract()

double refract	(	double	alt,
		double	temp,
		double	pressure
	)

◆ sgp4_init()

int sgp4_init	(	struct SGP4 *	sgp4,
		char **	errstr
	)

◆ sgp4_orbit()

double sgp4_orbit	(	struct SGP4 *	sgp4,
		struct TLE_VALUES *	tv,
		double	tsince
	)

◆ sgp4_pred()

int sgp4_pred	(	struct SGP4 *	sgp4,
		double	tsince,
		double	rect[6],
		char **	errstr
	)

◆ sgp4_tle()

int sgp4_tle	(	double *	epoch,
		struct SGP4 *	sgp4,
		char *	line1,
		char *	line2,
		char **	errstr
	)

◆ sunpos()

int sunpos	(	double	tjd,
		double	r[3],
		char **	errstr
	)

◆ tconv()

double tconv	(	double	tjd,
		char	conv[],
		char **	errstr
	)

◆ tcset()

int tcset	(	double	x,
		char	what[],
		char **	errstr
	)

◆ tle_parse()

int tle_parse	(	char *	line1,
		char *	line2,
		struct TLE_VALUES *	tv,
		char **	errstr
	)

◆ tmtojul()

double tmtojul ( struct tm * time )

Definition at line 32 of file time-utils.c.

◆ unrefract()

double unrefract	(	double	alt,
		double	temp,
		double	pressure
	)

Classes

Macros

Functions