# Made by “OrangeDog Team”
【Aircraft plugin】
File Name: dlc_aircraft_b787_ODp_v2.2.tme
File Introduction: Aerofly FS Global B787 parameter adjustment configuration file; customizable perspective (please refer to the guide below to modify it yourself); customizable load (fuel, passengers, cargo)
【Tutorial】
【Download】
【Parameter Tuning Guide】
Guide operation reminder:
This guide is made according to the needs of this plug-in and actual operation experience. It does not represent the official tutorial provided by Aerofly FS and may contain errors.
Do not modify or delete the code at will, otherwise it may cause serious crashes.
Access the configuration file:
The name of this plug-in is “dlc_dlc_aircraft_b787_ODp_v2.2.tme”. It is recommended to use “MT Manager“ for operation; other file management programs can also be used if they can run normally.
Click “dlc_dlc_aircraft_b787_ODp_v2.2.tme”, choose to open it as a compressed package, and open the “dlc_aircraft_b787”, “aircraft”, “b787”, and “b787_setting” folders in turn (that is, the path “dlc_aircraft_b787\aircraft\b787\b787_setting").
Click “parameters.tmd” and choose to open it in text format.
Please see below for specific parameter adjustment operations.
Load range:
max taxi = 254692 kg
max takeoff = 254011 kg
max landing = 201848 kg
max zero fuel = 192777 kg
operating empty = 135500 kg
min zero fuel = 110677 kg
max fuel = 101456 kg
max fuel (L/R) = 16716 kg (20895 lt) usable
max fuel (center) = 67653 kg (84566 lt) usable
max payload = 57277 kg
max cargp (fwd) = 36967 kg
max cargp (aft) = 30617 kg
max cargp (bulk) = 2735 kg
Fuel adjustment:
To change the fuel mass, modify the value of “fuel” directly below. center”, “fuel left”, “fuel right” in “Mass”; “LeftFuelMass” and “RightFuelMass” represent the total fuel volume of the left and right wings respectively; “GasoilInnerWingLeft” and “GasoilInnerWingRight” represent the inner fuel tanks of the left and right wings respectively, and the sum of the two values represents the total volume of the inner wing fuel tanks.
The mass of the center fuel tank when fully loaded is 67653kg.
The mass of the left wing tank and the right wing tank when fully loaded is 16716kg each.
Add the values of all fuel masses on the aircraft to get the total fuel volume of the aircraft, and fill in the values in the “BlockFuel” and “FuelOnBoard” rows under “fuel prediction”.
The unit of measurement is kilograms.
The value needs to be expressed as a real constant.
The full fuel mass is 102400.0kg.
It is recommended to refer to the manifest load and FCOM maximum takeoff weight and maximum landing weight (flight crew operating manual) for modifying the numerical value
Example (click the double arrows below to expand all codes):
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Passenger and cargo adjustment:
If you need to change the passenger mass, please directly modify the value corresponding to “Mass” in “payload” below.
If you need to change the cargo mass, please directly modify the value corresponding to “Mass” in “cargo” below.
The unit of measurement is kilograms.
The mass when empty is 1.0kg. (The value cannot be 0!)
The passenger mass when fully loaded is 31000.0kg.
The cargo mass when fully loaded is 56143.0kg.
It is recommended to refer to the manifest load and FCOM maximum takeoff weight and maximum landing weight (flight crew operating manual) for modifying the numerical value
Example (click the double arrows below to expand all codes):
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View adjustment:
[Overall structure]
The following is the view code structure in this plug-in, and some unnecessary codes have been removed.
Example (click the double arrows below to expand the full code):
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[View position]
The view position can be regarded as a spatial rectangular coordinate system with the center of the aircraft as the origin. α, β, and γ correspond to the X-axis, Y-axis, and Z-axis of the rectangular coordinate system. The positive direction of the X-axis is in front of the aircraft, the positive direction of the Y-axis is to the left of the aircraft, the positive direction of the X-axis is above the aircraft, the negative direction of the X-axis is behind the aircraft, the negative direction of the Y-axis is to the right of the aircraft, and the negative direction of the X-axis is below the aircraft.
The perspective “CameraPilot” does not display the captain model, and the cockpit is interactive; the perspective “CameraCopilot” displays the captain model, and the cockpit is interactive; the perspective “CameraJumpSeat” displays the captain model, and the cockpit is not interactive.
The value needs to be expressed as a real constant.
At least one space must be left before and after α, β, and γ.
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Example:
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[Viewing angle limit]
It is not recommended to modify the viewing angle limit, and please do not delete this line of code. This plugin will eliminate the viewing angle rotation limit by default, and the viewing angle rotation angle is not limited.
The value needs to be expressed as a real constant.
At least one space must be left before and after α, β, and γ.
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Example:
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[View direction]
View direction can be regarded as a spatial rectangular coordinate system with the view as the origin. α, β, γ correspond to the X-axis, Y-axis, and Z-axis of the spatial rectangular coordinate system. The positive direction of the X-axis is in front of the aircraft, the positive direction of the Y-axis is to the left of the aircraft, the positive direction of the X-axis is above the aircraft, the negative direction of the X-axis is behind the aircraft, the negative direction of the Y-axis is to the right of the aircraft, and the negative direction of the X-axis is below the aircraft.
The value needs to be expressed as a real constant.
At least one space must be left before and after α, β, and γ.
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Example:
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[View Type]
The content that can be filled in “xxx” is “true” or “false”. “True” means the view is from the cockpit, and “false” means the view is from outside the cabin. The sound effects of the cockpit and the cockpit are different.
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Example:
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Or:
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