P6DOF Atmosphere File Definition¶
A P6DOF atmosphere file defines five atmospheric properties:
Density versus altitude
Pressure versus altitude
Temperature versus altitude
Speed of sound versus altitude
Altitude band where contrailing may occur (optional)
The density, pressure, temperature, and speed of sound properties are defined in tables with altitude/data pairings. Altitude is measured in feet and data units are slugs/cu-ft (density), lbs/sq-ft (pressure), deg-Rankine (temperature), and ft/sec (speed of sound). Format is as follows:
p6dof_atmosphere
density_altitude_table
# altitude_ft density_slugs_ft3
0 0.002377170
1000 0.002308390
... ...
400000 0.000000000
end_density_altitude_table
pressure_altitude_table
# altitude_ft pressure_lbs_ft2
0 2116.2300
1000 2040.8600
... ...
400000 0.0000
end_pressure_altitude_table
temperature_altitude_table
# altitude_ft rankine_deg
0 518.67
1000 515.10
... ...
400000 336.50
end_temperature_altitude_table
sonic_speed_altitude_table
# altitude_ft sonic_speed_ft_s
0 1116.45
1000 1112.61
... ...
400000 899.27
end_sonic_speed_altitude_table
contrail_min_altitude_ ...
contrail_max_altitude_ ...
end_p6dof_atmosphere
For the tables, altitude must be listed in increasing values. It is recommended that the altitudes in the tables reach well beyond the maximum altitude of any P6DOF objects that will be used in the scenario. The practical limit of the atmosphere is between 300,000 to 400,000 feet, but the tables may go higher, if needed.
If contrailing conditions are present, the altitude band should be defined and must include both min and max altitudes, as follows:
- contrail_min_altitude <length-value>¶
This is the lowest altitude at which contrailing will occur.
- contrail_max_altitude <length-value>¶
This is the highest altitude at which contrailing will occur.
Return to p6dof_object_types or P6DOF Environment Support