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https://github.com/dcs-retribution/dcs-retribution.git
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fd473f0a46
Like with deleting waypoints, these will degrade the flight plan to the 2.1 behavior. Ascend/descend points aren't in use any more, so I removed those.
213 lines
8.2 KiB
Python
213 lines
8.2 KiB
Python
from __future__ import annotations
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import logging
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import math
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from datetime import timedelta
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from typing import Optional, TYPE_CHECKING
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from dcs.mapping import Point
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from dcs.unittype import FlyingType
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from game.utils import meter_to_nm
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from gen.flights.flight import Flight
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if TYPE_CHECKING:
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from gen.ato import Package
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class GroundSpeed:
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@classmethod
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def for_flight(cls, flight: Flight, altitude: int) -> int:
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if not issubclass(flight.unit_type, FlyingType):
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raise TypeError("Flight has non-flying unit")
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# TODO: Expose both a cruise speed and target speed.
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# The cruise speed can be used for ascent, hold, join, and RTB to save
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# on fuel, but mission speed will be fast enough to keep the flight
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# safer.
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c_sound_sea_level = 661.5
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# DCS's max speed is in kph at 0 MSL. Convert to knots.
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max_speed = flight.unit_type.max_speed * 0.539957
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if max_speed > c_sound_sea_level:
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# Aircraft is supersonic. Limit to mach 0.8 to conserve fuel and
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# account for heavily loaded jets.
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return int(cls.from_mach(0.8, altitude))
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# For subsonic aircraft, assume the aircraft can reasonably perform at
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# 80% of its maximum, and that it can maintain the same mach at altitude
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# as it can at sea level. This probably isn't great assumption, but
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# might. be sufficient given the wiggle room. We can come up with
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# another heuristic if needed.
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mach = max_speed * 0.8 / c_sound_sea_level
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return int(cls.from_mach(mach, altitude)) # knots
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@staticmethod
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def from_mach(mach: float, altitude: int) -> float:
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"""Returns the ground speed in knots for the given mach and altitude.
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Args:
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mach: The mach number to convert to ground speed.
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altitude: The altitude in feet.
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Returns:
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The ground speed corresponding to the given altitude and mach number
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in knots.
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"""
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# https://www.grc.nasa.gov/WWW/K-12/airplane/atmos.html
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if altitude <= 36152:
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temperature_f = 59 - 0.00356 * altitude
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else:
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# There's another formula for altitudes over 82k feet, but we better
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# not be planning waypoints that high...
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temperature_f = -70
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temperature_k = (temperature_f + 459.67) * (5 / 9)
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# https://www.engineeringtoolbox.com/specific-heat-ratio-d_602.html
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# Dependent on temperature, but varies very little (+/-0.001)
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# between -40F and 180F.
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heat_capacity_ratio = 1.4
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# https://www.grc.nasa.gov/WWW/K-12/airplane/sound.html
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gas_constant = 286 # m^2/s^2/K
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c_sound = math.sqrt(heat_capacity_ratio * gas_constant * temperature_k)
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# c_sound is in m/s, convert to knots.
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return (c_sound * 1.944) * mach
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class TravelTime:
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@staticmethod
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def between_points(a: Point, b: Point, speed: float) -> timedelta:
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error_factor = 1.1
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distance = meter_to_nm(a.distance_to_point(b))
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return timedelta(hours=distance / speed * error_factor)
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class TotEstimator:
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# An extra five minutes given as wiggle room. Expected to be spent at the
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# hold point performing any last minute configuration.
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HOLD_TIME = timedelta(minutes=5)
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def __init__(self, package: Package) -> None:
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self.package = package
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def mission_start_time(self, flight: Flight) -> timedelta:
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takeoff_time = self.takeoff_time_for_flight(flight)
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if takeoff_time is None:
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# Could not determine takeoff time, probably due to a custom flight
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# plan. Start immediately.
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return timedelta()
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startup_time = self.estimate_startup(flight)
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ground_ops_time = self.estimate_ground_ops(flight)
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start_time = takeoff_time - startup_time - ground_ops_time
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# In case FP math has given us some barely below zero time, round to
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# zero.
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if math.isclose(start_time.total_seconds(), 0):
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return timedelta()
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# Trim microseconds. DCS doesn't handle sub-second resolution for tasks,
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# and they're not interesting from a mission planning perspective so we
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# don't want them in the UI.
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#
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# Round down so *barely* above zero start times are just zero.
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return timedelta(seconds=math.floor(start_time.total_seconds()))
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def takeoff_time_for_flight(self, flight: Flight) -> Optional[timedelta]:
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travel_time = self.travel_time_to_rendezvous_or_target(flight)
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if travel_time is None:
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from gen.flights.flightplan import CustomFlightPlan
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if not isinstance(flight.flight_plan, CustomFlightPlan):
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logging.warning(
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"Found no rendezvous or target point. Cannot estimate "
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f"takeoff time takeoff time for {flight}.")
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return None
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from gen.flights.flightplan import FormationFlightPlan
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if isinstance(flight.flight_plan, FormationFlightPlan):
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tot = flight.flight_plan.tot_for_waypoint(
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flight.flight_plan.join)
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if tot is None:
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logging.warning(
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"Could not determine the TOT of the join point. Takeoff "
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f"time for {flight} will be immediate.")
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return None
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else:
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tot = self.package.time_over_target
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return tot - travel_time - self.HOLD_TIME
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def earliest_tot(self) -> timedelta:
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earliest_tot = max((
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self.earliest_tot_for_flight(f) for f in self.package.flights
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)) + self.HOLD_TIME
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# Trim microseconds. DCS doesn't handle sub-second resolution for tasks,
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# and they're not interesting from a mission planning perspective so we
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# don't want them in the UI.
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#
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# Round up so we don't get negative start times.
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return timedelta(seconds=math.ceil(earliest_tot.total_seconds()))
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def earliest_tot_for_flight(self, flight: Flight) -> timedelta:
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"""Estimate fastest time from mission start to the target position.
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For BARCAP flights, this is time to race track start. This ensures that
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they are on station at the same time any other package members reach
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their ingress point.
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For other mission types this is the time to the mission target.
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Args:
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flight: The flight to get the earliest TOT time for.
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Returns:
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The earliest possible TOT for the given flight in seconds. Returns 0
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if an ingress point cannot be found.
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"""
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time_to_target = self.travel_time_to_target(flight)
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if time_to_target is None:
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logging.warning(f"Cannot estimate TOT for {flight}")
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# Return 0 so this flight's travel time does not affect the rest
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# of the package.
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return timedelta()
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startup = self.estimate_startup(flight)
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ground_ops = self.estimate_ground_ops(flight)
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return startup + ground_ops + time_to_target
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@staticmethod
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def estimate_startup(flight: Flight) -> timedelta:
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if flight.start_type == "Cold":
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if flight.client_count:
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return timedelta(minutes=10)
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else:
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# The AI doesn't seem to have a real startup procedure.
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return timedelta(minutes=2)
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return timedelta()
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@staticmethod
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def estimate_ground_ops(flight: Flight) -> timedelta:
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if flight.start_type in ("Runway", "In Flight"):
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return timedelta()
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if flight.from_cp.is_fleet:
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return timedelta(minutes=2)
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else:
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return timedelta(minutes=5)
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@staticmethod
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def travel_time_to_target(flight: Flight) -> Optional[timedelta]:
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if flight.flight_plan is None:
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return None
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return flight.flight_plan.travel_time_to_target
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@staticmethod
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def travel_time_to_rendezvous_or_target(
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flight: Flight) -> Optional[timedelta]:
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if flight.flight_plan is None:
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return None
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from gen.flights.flightplan import FormationFlightPlan
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if isinstance(flight.flight_plan, FormationFlightPlan):
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return flight.flight_plan.travel_time_to_rendezvous
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return flight.flight_plan.travel_time_to_target
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