-- pg_orrery 0.1.0 -> 0.2.0 migration -- -- Phase 1: Stars, comets, and Keplerian propagation. -- Adds heliocentric type, star observation, and two-body propagation. -- ============================================================ -- Heliocentric type: ecliptic J2000 position in AU -- ============================================================ CREATE TYPE heliocentric; CREATE FUNCTION heliocentric_in(cstring) RETURNS heliocentric AS 'MODULE_PATHNAME' LANGUAGE C IMMUTABLE STRICT PARALLEL SAFE; CREATE FUNCTION heliocentric_out(heliocentric) RETURNS cstring AS 'MODULE_PATHNAME' LANGUAGE C IMMUTABLE STRICT PARALLEL SAFE; CREATE FUNCTION heliocentric_recv(internal) RETURNS heliocentric AS 'MODULE_PATHNAME' LANGUAGE C IMMUTABLE STRICT PARALLEL SAFE; CREATE FUNCTION heliocentric_send(heliocentric) RETURNS bytea AS 'MODULE_PATHNAME' LANGUAGE C IMMUTABLE STRICT PARALLEL SAFE; CREATE TYPE heliocentric ( INPUT = heliocentric_in, OUTPUT = heliocentric_out, RECEIVE = heliocentric_recv, SEND = heliocentric_send, INTERNALLENGTH = 24, ALIGNMENT = double, STORAGE = plain ); COMMENT ON TYPE heliocentric IS 'Heliocentric position in ecliptic J2000 frame (x, y, z in AU)'; CREATE FUNCTION helio_x(heliocentric) RETURNS float8 AS 'MODULE_PATHNAME' LANGUAGE C IMMUTABLE STRICT PARALLEL SAFE; COMMENT ON FUNCTION helio_x(heliocentric) IS 'X component in AU (ecliptic J2000, vernal equinox direction)'; CREATE FUNCTION helio_y(heliocentric) RETURNS float8 AS 'MODULE_PATHNAME' LANGUAGE C IMMUTABLE STRICT PARALLEL SAFE; COMMENT ON FUNCTION helio_y(heliocentric) IS 'Y component in AU (ecliptic J2000)'; CREATE FUNCTION helio_z(heliocentric) RETURNS float8 AS 'MODULE_PATHNAME' LANGUAGE C IMMUTABLE STRICT PARALLEL SAFE; COMMENT ON FUNCTION helio_z(heliocentric) IS 'Z component in AU (ecliptic J2000, north ecliptic pole)'; CREATE FUNCTION helio_distance(heliocentric) RETURNS float8 AS 'MODULE_PATHNAME' LANGUAGE C IMMUTABLE STRICT PARALLEL SAFE; COMMENT ON FUNCTION helio_distance(heliocentric) IS 'Heliocentric distance in AU'; -- ============================================================ -- Star observation functions -- ============================================================ CREATE FUNCTION star_observe(float8, float8, observer, timestamptz) RETURNS topocentric AS 'MODULE_PATHNAME' LANGUAGE C IMMUTABLE STRICT PARALLEL SAFE; COMMENT ON FUNCTION star_observe(float8, float8, observer, timestamptz) IS 'Observe a star from (ra_hours J2000, dec_degrees J2000, observer, time). Returns topocentric az/el. Range is 0 (infinite distance).'; CREATE FUNCTION star_observe_safe(float8, float8, observer, timestamptz) RETURNS topocentric AS 'MODULE_PATHNAME' LANGUAGE C IMMUTABLE PARALLEL SAFE; COMMENT ON FUNCTION star_observe_safe(float8, float8, observer, timestamptz) IS 'Like star_observe but returns NULL on invalid inputs. For batch queries over star catalogs.'; -- ============================================================ -- Keplerian propagation functions -- ============================================================ CREATE FUNCTION kepler_propagate( q_au float8, eccentricity float8, inclination_deg float8, arg_perihelion_deg float8, long_asc_node_deg float8, perihelion_jd float8, t timestamptz ) RETURNS heliocentric AS 'MODULE_PATHNAME' LANGUAGE C IMMUTABLE STRICT PARALLEL SAFE; COMMENT ON FUNCTION kepler_propagate(float8, float8, float8, float8, float8, float8, timestamptz) IS 'Two-body Keplerian propagation from classical orbital elements. Returns heliocentric ecliptic J2000 position in AU. Handles elliptic, parabolic, and hyperbolic orbits.'; -- ============================================================ -- Comet observation -- ============================================================ CREATE FUNCTION comet_observe( q_au float8, eccentricity float8, inclination_deg float8, arg_perihelion_deg float8, long_asc_node_deg float8, perihelion_jd float8, earth_x_au float8, earth_y_au float8, earth_z_au float8, obs observer, t timestamptz ) RETURNS topocentric AS 'MODULE_PATHNAME' LANGUAGE C IMMUTABLE STRICT PARALLEL SAFE; COMMENT ON FUNCTION comet_observe(float8, float8, float8, float8, float8, float8, float8, float8, float8, observer, timestamptz) IS 'Observe a comet/asteroid from orbital elements. Requires Earth heliocentric ecliptic J2000 position (AU). Returns topocentric az/el with geocentric range in km.'; -- ============================================================ -- Phase 2: VSOP87 planets, ELP82B Moon, Sun observation -- ============================================================ CREATE FUNCTION planet_heliocentric(int4, timestamptz) RETURNS heliocentric AS 'MODULE_PATHNAME' LANGUAGE C IMMUTABLE STRICT PARALLEL SAFE; COMMENT ON FUNCTION planet_heliocentric(int4, timestamptz) IS 'VSOP87 heliocentric ecliptic J2000 position (AU). Body IDs: 0=Sun, 1=Mercury, ..., 8=Neptune.'; CREATE FUNCTION planet_observe(int4, observer, timestamptz) RETURNS topocentric AS 'MODULE_PATHNAME' LANGUAGE C IMMUTABLE STRICT PARALLEL SAFE; COMMENT ON FUNCTION planet_observe(int4, observer, timestamptz) IS 'Observe a planet from (body_id 1-8, observer, time). Returns topocentric az/el with geocentric range in km.'; CREATE FUNCTION sun_observe(observer, timestamptz) RETURNS topocentric AS 'MODULE_PATHNAME' LANGUAGE C IMMUTABLE STRICT PARALLEL SAFE; COMMENT ON FUNCTION sun_observe(observer, timestamptz) IS 'Observe the Sun from (observer, time). Returns topocentric az/el with geocentric range in km.'; CREATE FUNCTION moon_observe(observer, timestamptz) RETURNS topocentric AS 'MODULE_PATHNAME' LANGUAGE C IMMUTABLE STRICT PARALLEL SAFE; COMMENT ON FUNCTION moon_observe(observer, timestamptz) IS 'Observe the Moon via ELP2000-82B from (observer, time). Returns topocentric az/el with geocentric range in km.'; -- ============================================================ -- Phase 3: Planetary moon observation -- ============================================================ CREATE FUNCTION galilean_observe(int4, observer, timestamptz) RETURNS topocentric AS 'MODULE_PATHNAME' LANGUAGE C IMMUTABLE STRICT PARALLEL SAFE; COMMENT ON FUNCTION galilean_observe(int4, observer, timestamptz) IS 'Observe a Galilean moon of Jupiter via L1.2 theory. Body IDs: 0=Io, 1=Europa, 2=Ganymede, 3=Callisto.'; CREATE FUNCTION saturn_moon_observe(int4, observer, timestamptz) RETURNS topocentric AS 'MODULE_PATHNAME' LANGUAGE C IMMUTABLE STRICT PARALLEL SAFE; COMMENT ON FUNCTION saturn_moon_observe(int4, observer, timestamptz) IS 'Observe a Saturn moon via TASS 1.7. Body IDs: 0=Mimas, 1=Enceladus, 2=Tethys, 3=Dione, 4=Rhea, 5=Titan, 6=Iapetus, 7=Hyperion.'; CREATE FUNCTION uranus_moon_observe(int4, observer, timestamptz) RETURNS topocentric AS 'MODULE_PATHNAME' LANGUAGE C IMMUTABLE STRICT PARALLEL SAFE; COMMENT ON FUNCTION uranus_moon_observe(int4, observer, timestamptz) IS 'Observe a Uranus moon via GUST86. Body IDs: 0=Miranda, 1=Ariel, 2=Umbriel, 3=Titania, 4=Oberon.'; CREATE FUNCTION mars_moon_observe(int4, observer, timestamptz) RETURNS topocentric AS 'MODULE_PATHNAME' LANGUAGE C IMMUTABLE STRICT PARALLEL SAFE; COMMENT ON FUNCTION mars_moon_observe(int4, observer, timestamptz) IS 'Observe a Mars moon via MarsSat. Body IDs: 0=Phobos, 1=Deimos.'; -- ============================================================ -- Phase 3: Jupiter decametric radio burst prediction -- ============================================================ CREATE FUNCTION io_phase_angle(timestamptz) RETURNS float8 AS 'MODULE_PATHNAME' LANGUAGE C IMMUTABLE STRICT PARALLEL SAFE; COMMENT ON FUNCTION io_phase_angle(timestamptz) IS 'Io orbital phase angle in degrees [0,360). 0=superior conjunction (behind Jupiter). Standard Radio JOVE convention.'; CREATE FUNCTION jupiter_cml(observer, timestamptz) RETURNS float8 AS 'MODULE_PATHNAME' LANGUAGE C IMMUTABLE STRICT PARALLEL SAFE; COMMENT ON FUNCTION jupiter_cml(observer, timestamptz) IS 'Jupiter Central Meridian Longitude, System III (1965.0), in degrees [0,360). Light-time corrected.'; CREATE FUNCTION jupiter_burst_probability(float8, float8) RETURNS float8 AS 'MODULE_PATHNAME' LANGUAGE C IMMUTABLE STRICT PARALLEL SAFE; COMMENT ON FUNCTION jupiter_burst_probability(float8, float8) IS 'Estimated Jupiter decametric burst probability (0-1) from (io_phase_deg, cml_deg). Based on Carr et al. (1983) source regions A, B, C, D.'; -- ============================================================ -- Phase 4: Interplanetary transfer orbits (Lambert solver) -- ============================================================ CREATE FUNCTION lambert_transfer( dep_body_id int4, arr_body_id int4, dep_time timestamptz, arr_time timestamptz, OUT c3_departure float8, OUT c3_arrival float8, OUT v_inf_departure float8, OUT v_inf_arrival float8, OUT tof_days float8, OUT transfer_sma float8 ) RETURNS RECORD AS 'MODULE_PATHNAME' LANGUAGE C IMMUTABLE STRICT PARALLEL SAFE; COMMENT ON FUNCTION lambert_transfer(int4, int4, timestamptz, timestamptz) IS 'Solve Lambert transfer between two planets. Returns C3 (km^2/s^2), v_infinity (km/s), TOF (days), SMA (AU). Body IDs 1-8.'; CREATE FUNCTION lambert_c3(int4, int4, timestamptz, timestamptz) RETURNS float8 AS 'MODULE_PATHNAME' LANGUAGE C IMMUTABLE STRICT PARALLEL SAFE; COMMENT ON FUNCTION lambert_c3(int4, int4, timestamptz, timestamptz) IS 'Departure C3 (km^2/s^2) for a Lambert transfer. Returns NULL if solver fails. For pork chop plots.';