Uses of Class
de.kah2.zodiac.nova4jmt.api.LnEllOrbit

Packages that use LnEllOrbit

Package	Description
de.kah2.zodiac.nova4jmt
de.kah2.zodiac.nova4jmt.solarsystem

Uses of LnEllOrbit in de.kah2.zodiac.nova4jmt

Methods in de.kah2.zodiac.nova4jmt with parameters of type LnEllOrbit

Modifier and Type	Method and Description
static double	EllipticMotion.ln_get_ell_body_earth_dist(double JD, LnEllOrbit orbit) double ln_get_ell_body_earth_dist(double JD, LnEllOrbit orbit) \param JD Julian day.
static double	EllipticMotion.ln_get_ell_body_elong(double JD, LnEllOrbit orbit) double ln_get_ell_body_elong(double JD, LnEllOrbit orbit); \param JD Julian day \param orbit Orbital parameters \return Elongation to the Sun.
static void	EllipticMotion.ln_get_ell_body_equ_coords(double JD, LnEllOrbit orbit, LnEquPosn posn) void ln_get_ell_body_equ_coords(double JD, LnEllOrbit orbit, LnEquPosn posn) \param JD Julian Day.
static int	EllipticMotion.ln_get_ell_body_next_rst_horizon_future(double JD, LnLnlatPosn observer, LnEllOrbit orbit, double horizon, int day_limit, LnRstTime rst) double ln_get_ell_body_next_rst_horizon(double JD, LnLnlatPosn observer, LnEllOrbit orbit, double horizon, LnRstTime rst); \param JD Julian day \param observer Observers position \param orbit Orbital parameters \param horizon Horizon height \param day_limit Maximal number of days that will be searched for next rise and set \param rst Pointer to store Rise, Set and Transit time in JD \return 0 for success, else 1 for circumpolar (above the horizon), -1 for circumpolar (bellow the horizon) Calculate the time of next rise, set and transit (crosses the local meridian at upper culmination) time of a body with an elliptic orbit for the given Julian day.
static int	EllipticMotion.ln_get_ell_body_next_rst_horizon(double JD, LnLnlatPosn observer, LnEllOrbit orbit, double horizon, LnRstTime rst) double ln_get_ell_body_next_rst_horizon(double JD, LnLnlatPosn observer, LnEllOrbit orbit, double horizon, LnRstTime rst); \param JD Julian day \param observer Observers position \param orbit Orbital parameters \param horizon Horizon height \param rst Pointer to store Rise, Set and Transit time in JD \return 0 for success, else 1 for circumpolar (above the horizon), -1 for circumpolar (bellow the horizon) Calculate the time of next rise, set and transit (crosses the local meridian at upper culmination) time of a body with an elliptic orbit for the given Julian day.
static int	EllipticMotion.ln_get_ell_body_next_rst(double JD, LnLnlatPosn observer, LnEllOrbit orbit, LnRstTime rst) double ln_get_ell_body_next_rst(double JD, LnLnlatPosn observer, LnEllOrbit orbit, LnRstTime rst); \param JD Julian day \param observer Observers position \param orbit Orbital parameters \param rst Pointer to store Rise, Set and Transit time in JD \return 0 for success, else 1 for circumpolar (above the horizon), -1 for circumpolar (bellow the horizon) Calculate the time of next rise, set and transit (crosses the local meridian at upper culmination) time of a body with an elliptic orbit for the given Julian day.
static double	EllipticMotion.ln_get_ell_body_phase_angle(double JD, LnEllOrbit orbit) double ln_get_ell_body_phase_angle(double JD, LnEllOrbit orbit); \param JD Julian day \param orbit Orbital parameters \return Phase angle.
static int	EllipticMotion.ln_get_ell_body_rst_horizon(double JD, LnLnlatPosn observer, LnEllOrbit orbit, double horizon, LnRstTime rst) double ln_get_ell_body_rst_horizon(double JD, LnLnlatPosn observer, LnEllOrbit orbit, double horizon, LnRstTime rst); \param JD Julian day \param observer Observers position \param orbit Orbital parameters \param horizon Horizon height \param rst Pointer to store Rise, Set and Transit time in JD \return 0 for success, else 1 for circumpolar (above the horizon), -1 for circumpolar (bellow the horizon) Calculate the time the rise, set and transit (crosses the local meridian at upper culmination) time of a body with an elliptic orbit for the given Julian day.
static int	EllipticMotion.ln_get_ell_body_rst(double JD, LnLnlatPosn observer, LnEllOrbit orbit, LnRstTime rst) double ln_get_ell_body_rst(double JD, LnLnlatPosn observer, LnEllOrbit orbit, LnRstTime rst); \param JD Julian day \param observer Observers position \param orbit Orbital parameters \param rst Pointer to store Rise, Set and Transit time in JD \return 0 for success, else 1 for circumpolar (above the horizon), -1 for circumpolar (bellow the horizon) Calculate the time the rise, set and transit (crosses the local meridian at upper culmination) time of a body with an elliptic orbit for the given Julian day.
static double	EllipticMotion.ln_get_ell_body_solar_dist(double JD, LnEllOrbit orbit) double ln_get_ell_body_solar_dist(double JD, LnEllOrbit orbit) \param JD Julian Day.
static void	EllipticMotion.ln_get_ell_geo_rect_posn(LnEllOrbit orbit, double JD, LnRectPosn posn) void ln_get_ell_geo_rect_posn(LnEllOrbit orbit, double JD, LnRectPosn posn); \param orbit Orbital parameters of object.
static void	EllipticMotion.ln_get_ell_helio_rect_posn(LnEllOrbit orbit, double JD, LnRectPosn posn) void ln_get_ell_helio_rect_posn(LnEllOrbit orbit, double JD, LnRectPosn posn); \param orbit Orbital parameters of object.
static double	EllipticMotion.ln_get_ell_orbit_avel(LnEllOrbit orbit) double ln_get_ell_orbit_avel(LnEllOrbit orbit); \param orbit Orbital parameters \return Orbital velocity in km/s.
static double	EllipticMotion.ln_get_ell_orbit_len(LnEllOrbit orbit) double ln_get_ell_orbit_len(LnEllOrbit orbit); \param orbit Orbital parameters \return Orbital length in AU Calculate the orbital length in AU.
static double	EllipticMotion.ln_get_ell_orbit_pvel(LnEllOrbit orbit) double ln_get_ell_orbit_pvel(LnEllOrbit orbit); \param orbit Orbital parameters \return Orbital velocity in km/s.
static double	EllipticMotion.ln_get_ell_orbit_vel(double JD, LnEllOrbit orbit) double ln_get_ell_orbit_vel(double JD, LnEllOrbit orbit); \param JD Julian day.

Uses of LnEllOrbit in de.kah2.zodiac.nova4jmt.solarsystem

Methods in de.kah2.zodiac.nova4jmt.solarsystem with parameters of type LnEllOrbit

Modifier and Type	Method and Description
static double	Asteroid.ln_get_asteroid_mag(double JD, LnEllOrbit orbit, double H, double G) double ln_get_asteroid_mag(double JD, LnEllOrbit orbit, double H, double G) \param JD Julian day.
static double	Asteroid.ln_get_asteroid_sdiam_arc(double JD, LnEllOrbit orbit, double H, double A) double ln_get_asteroid_sdiam_arc(double JD, LnEllOrbit orbit, double H, double A) \param JD Julian day \param orbit Orbital parameters \param H Absolute magnitude of asteroid \param A Albedo of asteroid \return Semidiameter in seconds of arc Calculate the semidiameter of an asteroid in arc seconds.
static double	Comet.ln_get_ell_comet_mag(double JD, LnEllOrbit orbit, double g, double k) double ln_get_ell_comet_mag(double JD, LnEllOrbit orbit, double g, double k) \param JD Julian day.