from pyModeS import adsb from pytest import approx # === TEST ADS-B package === def test_adsb_icao(): assert adsb.icao("8D406B902015A678D4D220AA4BDA") == "406B90" def test_adsb_category(): assert adsb.category("8D406B902015A678D4D220AA4BDA") == 0 def test_adsb_callsign(): assert adsb.callsign("8D406B902015A678D4D220AA4BDA") == "EZY85MH_" def test_adsb_position(): pos = adsb.position( "8D40058B58C901375147EFD09357", "8D40058B58C904A87F402D3B8C59", 1446332400, 1446332405, ) assert pos == (approx(49.81755, 0.001), approx(6.08442, 0.001)) def test_adsb_position_swap_odd_even(): pos = adsb.position( "8D40058B58C904A87F402D3B8C59", "8D40058B58C901375147EFD09357", 1446332405, 1446332400, ) assert pos == (approx(49.81755, 0.001), approx(6.08442, 0.001)) def test_adsb_position_with_ref(): pos = adsb.position_with_ref("8D40058B58C901375147EFD09357", 49.0, 6.0) assert pos == (approx(49.82410, 0.001), approx(6.06785, 0.001)) pos = adsb.position_with_ref("8FC8200A3AB8F5F893096B000000", -43.5, 172.5) assert pos == (approx(-43.48564, 0.001), approx(172.53942, 0.001)) def test_adsb_airborne_position_with_ref(): pos = adsb.airborne_position_with_ref( "8D40058B58C901375147EFD09357", 49.0, 6.0 ) assert pos == (approx(49.82410, 0.001), approx(6.06785, 0.001)) pos = adsb.airborne_position_with_ref( "8D40058B58C904A87F402D3B8C59", 49.0, 6.0 ) assert pos == (approx(49.81755, 0.001), approx(6.08442, 0.001)) def test_adsb_surface_position_with_ref(): pos = adsb.surface_position_with_ref( "8FC8200A3AB8F5F893096B000000", -43.5, 172.5 ) assert pos == (approx(-43.48564, 0.001), approx(172.53942, 0.001)) def test_adsb_surface_position(): pos = adsb.surface_position( "8CC8200A3AC8F009BCDEF2000000", "8FC8200A3AB8F5F893096B000000", 0, 2, -43.496, 172.558, ) assert pos == (approx(-43.48564, 0.001), approx(172.53942, 0.001)) def test_adsb_alt(): assert adsb.altitude("8D40058B58C901375147EFD09357") == 39000 def test_adsb_velocity(): vgs = adsb.velocity("8D485020994409940838175B284F") vas = adsb.velocity("8DA05F219B06B6AF189400CBC33F") vgs_surface = adsb.velocity("8FC8200A3AB8F5F893096B000000") assert vgs == (159, approx(182.88, 0.1), -832, "GS") assert vas == (375, approx(243.98, 0.1), -2304, "TAS") assert vgs_surface == (19, approx(42.2, 0.1), 0, "GS") assert adsb.altitude_diff("8D485020994409940838175B284F") == 550 def test_adsb_emergency(): assert not adsb.is_emergency("8DA2C1B6E112B600000000760759") assert adsb.emergency_state("8DA2C1B6E112B600000000760759") == 0 assert adsb.emergency_squawk("8DA2C1B6E112B600000000760759") == "6513" def test_adsb_target_state_status(): sel_alt = adsb.selected_altitude("8DA05629EA21485CBF3F8CADAEEB") assert sel_alt == (16992, "MCP/FCU") assert adsb.baro_pressure_setting("8DA05629EA21485CBF3F8CADAEEB") == 1012.8 assert adsb.selected_heading("8DA05629EA21485CBF3F8CADAEEB") == approx( 66.8, 0.1 ) assert adsb.autopilot("8DA05629EA21485CBF3F8CADAEEB") is True assert adsb.vnav_mode("8DA05629EA21485CBF3F8CADAEEB") is True assert adsb.altitude_hold_mode("8DA05629EA21485CBF3F8CADAEEB") is False assert adsb.approach_mode("8DA05629EA21485CBF3F8CADAEEB") is False assert adsb.tcas_operational("8DA05629EA21485CBF3F8CADAEEB") is True assert adsb.lnav_mode("8DA05629EA21485CBF3F8CADAEEB") is True # def test_nic(): # assert adsb.nic('8D3C70A390AB11F55B8C57F65FE6') == 0 # assert adsb.nic('8DE1C9738A4A430B427D219C8225') == 1 # assert adsb.nic('8D44058880B50006B1773DC2A7E9') == 2 # assert adsb.nic('8D44058881B50006B1773DC2A7E9') == 3 # assert adsb.nic('8D4AB42A78000640000000FA0D0A') == 4 # assert adsb.nic('8D4405887099F5D9772F37F86CB6') == 5 # assert adsb.nic('8D4841A86841528E72D9B472DAC2') == 6 # assert adsb.nic('8D44057560B9760C0B840A51C89F') == 7 # assert adsb.nic('8D40621D58C382D690C8AC2863A7') == 8 # assert adsb.nic('8F48511C598D04F12CCF82451642') == 9 # assert adsb.nic('8DA4D53A50DBF8C6330F3B35458F') == 10 # assert adsb.nic('8D3C4ACF4859F1736F8E8ADF4D67') == 11