def test_engines(self):
"""Test that engines use fuel and accelerate at the expected."""
with PhysicsEngine('tests/habitat.json') as physics_engine:
# In this test case, there is a single entity that has 300 kg fuel.
# heading, velocity, and position are all 0.
throttle = 1
t_delta = 5
physics_engine.handle_requests([
network.Request(ident=network.Request.HAB_THROTTLE_SET,
throttle_set=throttle)
],
requested_t=0)
initial = physics_engine.get_state(0)
moved = physics_engine.get_state(t_delta)
self.assertAlmostEqual(initial[0].heading, 0)
self.assertAlmostEqual(
moved[0].fuel, (initial[0].fuel - t_delta * throttle *
common.craft_capabilities[HABITAT].fuel_cons))
self.assertTrue(
moved[0].vx < (t_delta * calc.engine_acceleration(moved)))
t_no_fuel = (
initial[0].fuel /
(throttle * common.craft_capabilities[HABITAT].fuel_cons))
empty_fuel = physics_engine.get_state(t_no_fuel)
after_empty_fuel = physics_engine.get_state(t_no_fuel + t_delta)
self.assertEqual(round(empty_fuel[0].fuel), 0)
self.assertEqual(round(after_empty_fuel[0].vx),
round(empty_fuel[0].vx))
def test_srbs(self):
"""Test that SRBs move the craft, and run out of fuel."""
with PhysicsEngine('tests/habitat.json') as physics_engine:
t_delta = 5
physics_engine.handle_requests(
[network.Request(ident=network.Request.IGNITE_SRBS)],
requested_t=0)
initial = physics_engine.get_state(0)
moved = physics_engine.get_state(t_delta)
self.assertAlmostEqual(initial[0].heading, 0)
self.assertAlmostEqual(initial[0].vx, 0)
self.assertAlmostEqual(moved[0].vx,
t_delta * calc.engine_acceleration(moved))
srb_empty = physics_engine.get_state(common.SRB_BURNTIME)
after_srb_empty = physics_engine.get_state(common.SRB_BURNTIME + 5)
self.assertAlmostEqual(srb_empty[0].vx, after_srb_empty[0].vx)
def _create_wtexts(self):
vpython.canvas.get_selected().caption += "<table>\n"
self._wtexts: List[TableText] = []
self._wtexts.append(
TableText("Simulation time",
lambda state: datetime.fromtimestamp(
state.timestamp, common.TIMEZONE).strftime('%x %X'),
"Current time in simulation",
new_section=False))
self._wtexts.append(
TableText("Orbit speed",
lambda state: common.format_num(
calc.orb_speed(state.craft_entity(),
state.reference_entity()), " m/s"),
"Speed required for circular orbit at current altitude",
new_section=False))
self._wtexts.append(
TableText(
"Periapsis",
lambda state: common.format_num(calc.periapsis(
state.craft_entity(), state.reference_entity()) / 1000,
" km",
decimals=3),
"Lowest altitude in naïve orbit around reference",
new_section=False))
self._wtexts.append(
TableText(
"Apoapsis",
lambda state: common.format_num(calc.apoapsis(
state.craft_entity(), state.reference_entity()) / 1000,
" km",
decimals=3),
"Highest altitude in naïve orbit around reference",
new_section=False))
self._wtexts.append(
TableText(
# The H in HRT stands for Habitat, even though craft is more
# general and covers Ayse, but HRT is the familiar triple name and
# the Hawking III says trans rights.
"HRT phase θ",
lambda state: common.format_num(
calc.phase_angle(
state.craft_entity(), state.reference_entity(),
state.target_entity()), "°") or "Same ref and targ",
"Angle between Habitat, Reference, and Target",
new_section=False))
self._wtexts.append(
TableText(
"Throttle",
lambda state: "{:.1%}".format(state.craft_entity().throttle),
"Percentage of habitat's maximum rated engines",
new_section=True))
self._wtexts.append(
TableText("Engine Acceleration",
lambda state: common.format_num(
calc.engine_acceleration(state), " m/s/s") +
(' [SRB]' if state.srb_time > 0 else ''),
"Acceleration due to craft's engine thrust",
new_section=False))
self._wtexts.append(
TableText("Drag",
lambda state: common.format_num(
calc.fastnorm(calc.drag(state)), " m/s/s"),
"Atmospheric drag acting on the craft",
new_section=False))
self._wtexts.append(
TableText("Fuel",
lambda state: common.format_num(
state.craft_entity().fuel, " kg"),
"Remaining fuel of craft",
new_section=False))
def rotation_formatter(state: PhysicsState) -> str:
deg_spin = round(np.degrees(state.craft_entity().spin), ndigits=1)
if deg_spin < 0:
return f"{-deg_spin} °/s cw"
elif deg_spin > 0:
return f"{deg_spin} °/s ccw"
else:
return f"{deg_spin} °/s"
self._wtexts.append(
TableText("Rotation",
rotation_formatter,
"Rotation speed of craft",
new_section=False))
self._wtexts.append(
TableText(
"Ref altitude",
lambda state: common.format_num(calc.altitude(
state.craft_entity(), state.reference_entity()) / 1000,
" km",
decimals=3),
"Altitude of habitat above reference surface",
new_section=True))
self._wtexts.append(
TableText("Ref speed",
lambda state: common.format_num(
calc.speed(state.craft_entity(),
state.reference_entity()), " m/s"),
"Speed of habitat above reference surface",
new_section=False))
self._wtexts.append(
TableText(
"Vertical speed",
lambda state: common.format_num(
calc.v_speed(state.craft_entity(), state.reference_entity(
)), " m/s "),
"Vertical speed of habitat towards/away reference surface",
new_section=False))
self._wtexts.append(
TableText("Horizontal speed",
lambda state: common.format_num(
calc.h_speed(state.craft_entity(),
state.reference_entity()), " m/s "),
"Horizontal speed of habitat across reference surface",
new_section=False))
self._wtexts.append(
TableText("Pitch θ",
lambda state: common.format_num(
np.degrees(
calc.pitch(state.craft_entity(
), state.reference_entity())) % 360, "°"),
"Horizontal speed of habitat across reference surface",
new_section=False))
self._wtexts.append(
TableText("Targ altitude",
lambda state: common.format_num(calc.altitude(
state.craft_entity(), state.target_entity()) / 1000,
" km",
decimals=3),
"Altitude of habitat above reference surface",
new_section=True))
self._wtexts.append(
TableText("Targ speed",
lambda state: common.format_num(
calc.speed(state.craft_entity(), state.target_entity(
)), " m/s"),
"Speed of habitat above target surface",
new_section=False))
self._wtexts.append(
TableText(
"Landing acc",
lambda state: common.format_num(
calc.landing_acceleration(state.craft_entity(),
state.target_entity()), " m/s/s"
) or "no vertical landing",
"Constant engine acc to land during vertical descent to target",
new_section=False))
vpython.canvas.get_selected().caption += "</table>"
