def test_orbit_kerbin(self): load_save("orbit-kerbin") ksp = krpc.connect() vessel = ksp.space_center.active_vessel orbit = vessel.orbit # inc 0 # e 0 # sma 70000 # lan 0 # w 0 # mEp 0 # epoch 0 # body Kerbin self.assertEqual("Kerbin", orbit.body.name) self.assertClose(100000 + 600000, orbit.apoapsis, error=10) self.assertClose(100000 + 600000, orbit.periapsis, error=10) self.assertClose(100000, orbit.apoapsis_altitude, error=10) self.assertClose(100000, orbit.periapsis_altitude, error=10) self.assertClose(100000 + 600000, orbit.semi_major_axis, error=10) self.assertClose(100000, orbit.semi_major_axis_altitude, error=10) self.assertClose(700000, orbit.radius, error=10) self.assertClose(2246.1, orbit.speed, error=1) self.assertClose(603.48, orbit.time_to_apoapsis, error=1) self.assertClose(1582.5, orbit.time_to_periapsis, error=1) self.assertTrue(math.isnan(orbit.time_to_soi_change)) self.assertClose(0, orbit.eccentricity, error=0.1) self.assertClose(0, orbit.inclination, error=0.1) self.assertClose(0, orbit.longitude_of_ascending_node, error=0.1) self.assertClose(0, orbit.argument_of_periapsis, error=0.1) self.assertClose(0, orbit.mean_anomaly_at_epoch, error=0.1) self.assertEqual(None, orbit.next_orbit)
def setUp(self): load_save('autopilot') self.conn = krpc.connect() self.vessel = self.conn.space_center.active_vessel self.ref = self.conn.space_center.ReferenceFrame self.ap = self.vessel.auto_pilot self.vessel.control.sas = False
def test_orbit_bop(self): load_save("orbit-bop") ksp = krpc.connect() vessel = ksp.space_center.active_vessel orbit = vessel.orbit # inc 27 # e 0.18 # sma 320000 # lan 38 # w 241 # mEp 2.3 # epoch 0 # body Kerbin self.assertEqual("Bop", orbit.body.name) self.assertClose(377600, orbit.apoapsis, error=10) self.assertClose(262400, orbit.periapsis, error=10) self.assertClose(377600 - 65000, orbit.apoapsis_altitude, error=10) self.assertClose(262400 - 65000, orbit.periapsis_altitude, error=10) self.assertClose(0.5 * (377600 + 262400), orbit.semi_major_axis, error=10) self.assertClose(0.5 * (377600 - 65000 + 262400 - 65000), orbit.semi_major_axis_altitude, error=10) self.assertClose(366329, orbit.radius, error=10) self.assertClose(76, orbit.speed, error=1) self.assertClose(2698.33, orbit.time_to_apoapsis, error=1) self.assertClose(14102.17, orbit.time_to_periapsis, error=1) self.assertTrue(math.isnan(orbit.time_to_soi_change)) self.assertClose(0.18, orbit.eccentricity, error=0.1) self.assertClose(27, orbit.inclination, error=0.1) self.assertClose(38, orbit.longitude_of_ascending_node, error=0.1) self.assertClose(241, orbit.argument_of_periapsis, error=0.1) self.assertClose(2.3, orbit.mean_anomaly_at_epoch, error=0.1) self.assertEqual(None, orbit.next_orbit)
def setUp(self): load_save('autopilot') self.conn = krpc.connect() self.vessel = self.conn.space_center.active_vessel self.ap = self.vessel.auto_pilot self.sas_mode = self.conn.space_center.SASMode self.speed_mode = self.conn.space_center.SpeedMode
def setUpClass(cls): load_save('flight') cls.conn = krpc.connect() cls.ref = cls.conn.space_center.ReferenceFrame cls.vessel = cls.conn.space_center.active_vessel cls.surface_flight = cls.vessel.flight(cls.ref.surface) cls.orbital_flight = cls.vessel.flight(cls.ref.orbital) cls.maneuver_flight = cls.vessel.flight(cls.ref.maneuver)
def test_orbit_mun_escape_soi(self): load_save("orbit-mun-escape-soi") ksp = krpc.connect() vessel = ksp.space_center.active_vessel orbit = vessel.orbit # inc 0 # e 0.52 # sma 1800000 # lan 13 # w 67 # mEp 6.25 # epoch 0 # body Mun self.assertEqual("Mun", orbit.body.name) self.assertClose(2736000, orbit.apoapsis, error=10) self.assertClose(864000, orbit.periapsis, error=10) self.assertClose(2736000 - 200000, orbit.apoapsis_altitude, error=10) self.assertClose(864000 - 200000, orbit.periapsis_altitude, error=10) self.assertClose(0.5 * (2736000 + 864000), orbit.semi_major_axis, error=10) self.assertClose(0.5 * (2736000 - 200000 + 864000 - 200000), orbit.semi_major_axis_altitude, error=10) self.assertClose(865546, orbit.radius, error=10) self.assertClose(338.1, orbit.speed, error=1) self.assertClose(29987.92, orbit.time_to_apoapsis, error=1) self.assertClose(261.65, orbit.time_to_periapsis, error=1) self.assertClose(18464, orbit.time_to_soi_change, error=5) self.assertClose(0.52, orbit.eccentricity, error=0.1) self.assertClose(0, orbit.inclination, error=0.1) # TODO: fix this # self.assertClose(13, orbit.longitude_of_ascending_node, error=0.1) # self.assertClose(67, orbit.argument_of_periapsis, error=0.1) # self.assertClose(6.2, orbit.mean_anomaly_at_epoch, error=0.1) self.assertTrue(orbit.next_orbit is not None) orbit = orbit.next_orbit self.assertEqual("Kerbin", orbit.body.name) self.assertClose(25224000, orbit.apoapsis, error=1000) self.assertClose(12428000, orbit.periapsis, error=1000)
def setUpClass(cls): load_save('basic') cls.conn = krpc.connect()
def setUpClass(cls): load_save('orbit-kerbin') cls.conn = krpc.connect() cls.vessel = cls.conn.space_center.active_vessel cls.control = cls.vessel.control
def setUpClass(cls): load_save('resources') cls.conn = krpc.connect() cls.r = cls.conn.space_center.active_vessel.resources
def setUpClass(cls): load_save('control') cls.conn = krpc.connect() cls.control = cls.conn.space_center.active_vessel.control vessel = cls.conn.space_center.active_vessel cls.orbital_flight = vessel.flight(cls.conn.space_center.ReferenceFrame.orbital)