pg_orrery/Makefile
Ryan Malloy 70420c3b4f Phase 4: Lambert transfer orbit solver for interplanetary trajectories
Add Universal Variable Lambert solver for computing transfer orbits
between any two planets. Enables pork chop plot generation as SQL:

  SELECT dep_date, arr_date, lambert_c3(3, 4, dep_date, arr_date)
  FROM generate_series(...) dep CROSS JOIN generate_series(...) arr;

New functions:
- lambert_transfer(dep_body, arr_body, dep_time, arr_time) → RECORD
  Returns C3 departure/arrival (km^2/s^2), v_infinity (km/s),
  time of flight (days), and transfer orbit SMA (AU).
- lambert_c3(dep_body, arr_body, dep_time, arr_time) → float8
  Convenience: departure C3 only, NULL on solver failure.

The solver uses Stumpff functions for unified elliptic/parabolic/hyperbolic
handling, with Newton-Raphson iteration and bisection fallback.
Each solve is sub-millisecond; PARALLEL SAFE for batch computation.

All 11 regression tests pass.
2026-02-16 02:00:09 -07:00

74 lines
2.7 KiB
Makefile

MODULE_big = pg_orbit
EXTENSION = pg_orbit
DATA = sql/pg_orbit--0.1.0.sql sql/pg_orbit--0.2.0.sql sql/pg_orbit--0.1.0--0.2.0.sql
# Our extension C sources
OBJS = src/pg_orbit.o src/tle_type.o src/eci_type.o src/observer_type.o \
src/sgp4_funcs.o src/coord_funcs.o src/pass_funcs.o src/gist_tle.o \
src/star_funcs.o src/kepler_funcs.o \
src/vsop87.o src/elp82b.o src/elliptic_to_rectangular.o \
src/precession.o src/sidereal_time.o src/planet_funcs.o \
src/tass17.o src/gust86.o src/marssat.o src/l12.o \
src/moon_funcs.o src/radio_funcs.o \
src/lambert.o src/transfer_funcs.o
# sat_code C++ sources (compiled with g++, linked with extern "C" symbols)
SAT_CODE_DIR = lib/sat_code
SAT_CODE_SRCS = $(SAT_CODE_DIR)/sgp4.cpp $(SAT_CODE_DIR)/sdp4.cpp \
$(SAT_CODE_DIR)/deep.cpp $(SAT_CODE_DIR)/common.cpp \
$(SAT_CODE_DIR)/basics.cpp $(SAT_CODE_DIR)/get_el.cpp \
$(SAT_CODE_DIR)/tle_out.cpp
SAT_CODE_OBJS = $(SAT_CODE_SRCS:.cpp=.o)
OBJS += $(SAT_CODE_OBJS)
# Regression tests
REGRESS = tle_parse sgp4_propagate coord_transforms pass_prediction gist_index convenience \
star_observe kepler_comet planet_observe moon_observe lambert_transfer
REGRESS_OPTS = --inputdir=test
# Need C++ runtime for sat_code
SHLIB_LINK += -lstdc++ -lm
# Compiler flags
PG_CPPFLAGS = -I$(SAT_CODE_DIR)
# Use PGXS
PG_CONFIG ?= pg_config
PGXS := $(shell $(PG_CONFIG) --pgxs)
include $(PGXS)
# Rule for compiling sat_code C++ files
$(SAT_CODE_DIR)/%.o: $(SAT_CODE_DIR)/%.cpp
$(CXX) $(CXXFLAGS) -fPIC -I$(SAT_CODE_DIR) -c -o $@ $<
# ── Docker packaging ────────────────────────────────────────
REGISTRY ?= git.supported.systems/warehack.ing
IMAGE ?= pg_orbit
PG_MAJOR ?= 17
TAG ?= pg$(PG_MAJOR)
docker-build:
docker build --build-arg PG_MAJOR=$(PG_MAJOR) \
--target artifact -t $(REGISTRY)/$(IMAGE):$(TAG)-artifact .
docker build --build-arg PG_MAJOR=$(PG_MAJOR) \
--target standalone -t $(REGISTRY)/$(IMAGE):$(TAG) .
docker-push:
docker push $(REGISTRY)/$(IMAGE):$(TAG)-artifact
docker push $(REGISTRY)/$(IMAGE):$(TAG)
docker-test:
@echo "Smoke-testing standalone image..."
docker run --rm -d --name pg_orbit_test \
-e POSTGRES_PASSWORD=test $(REGISTRY)/$(IMAGE):$(TAG)
@echo "Waiting for PostgreSQL to initialize..."
@sleep 10
docker exec pg_orbit_test psql -U postgres -tAc \
"SELECT tle_norad_id(E'1 25544U 98067A 24001.50000000 .00016717 00000-0 10270-3 0 9025\n2 25544 51.6400 208.9163 0006703 30.1694 61.7520 15.50100486 00001'::tle);" \
| grep -q 25544
@docker stop pg_orbit_test
@echo "Smoke test passed."
.PHONY: docker-build docker-push docker-test