A380 Enhanced Plugin | ACC Aero Center

# Made by “OrangeDog Team”

【Aircraft plugin】

File Name: dlc_aircraft_a380_ODp_v4.2.tme

File Introduction: Aerofly FS Global A380 parameter adjustment configuration file; customizable perspective (please refer to the guide below to modify it yourself); customizable load (fuel, passengers)

【Tutorial】

Install Tutorial

【Download】

Download in “Terabox”

【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_a380_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_a380_ODp_v2.2.tme”, choose to open it in the form of a compressed package, and open the “dlc_aircraft_a380”, “aircraft”, “a380”, and “a380_setting” folders in turn (that is, the path “dlc_aircraft_a380\aircraft\a380\a380_setting").
Click “parameters.tmd” and choose to open it in text format.
Please see below for specific parameter adjustment operations.

Fuel adjustment:

If you need to change the fuel mass, please directly modify the value corresponding to “Mass” in “fuel left” and “fuel right” below; “GasoilInnerWingLeft” and “GasoilOuterWingLeft” represent the inner and outer fuel tanks of the left wing respectively, and the sum of the two values represents the total amount of the left wing fuel tank; “GasoilInnerWingRight” and “FuelOuterWingRight” represent the inner and outer fuel tanks of the right wing respectively, and the sum of the two values represents the total mass of the right wing fuel tank.

The mass of the left wing inner fuel tank when fully loaded is 162000.0kg.

The mass of the left wing outer fuel tank when fully loaded is 10500.0kg.

The mass of the right wing inner fuel tank when fully loaded is 162000.0kg.

The mass of the right wing external fuel tank when fully loaded is 10500.0kg.

Add the values of all the fuel masses on the aircraft to get the total fuel load of the aircraft. Fill in the values in the “BlockFuel” and “FuelOnBoard” rows under “fuel prediction”.

The unit of measurement is kilograms.

The values need to be expressed as real constants.

It is recommended to refer to the manifest load and FCOM maximum takeoff weight (flight crew operating manual) for modifying the numerical value

Example (click the double arrows below to expand all codes):


// fuel left

<[rigidbody][GasoilInnerWingLeft][]
<[float64][Mass][80000.0]>
>
<[rigidbody][GasoilOuterWingLeft][]
<[float64][Mass][5000.0]>
>

// fuel right

<[rigidbody][GasoilInnerWingRight][]
<[float64][Mass][80000.0]>
>
<[rigidbody][GasoilOuterWingRight][]
<[float64][Mass][5000.0]>
>

//fuel_prediction

<[fuel_prediction][FuelPrediction][]
<[float64][ZeroFuelMass] [360000.0]> // Zero fuel weight = aircraft weight 167832.0kg + payload mass
<[float64][BlockFuel] [100000.0]> // Fuel tank weight data
<[float64][FuelOnBoard] [120000.0]> // MCDU fuel weight data
<[float64][TaxiFuel] [ 600.0]> // Taxi fuel volume, it is recommended to keep the default value
>

Passenger load adjustment:

If you need to change the passenger mass, please directly modify the value corresponding to “Mass” in “payload” below; “InertiaLength” indicates mass distribution, which will affect the center of gravity, and it is not recommended to modify it.

The unit of measurement is kilograms.

The mass when empty is 1.0kg. (The value cannot be 0!)

Load = (Number of passengers + Number of crew members) x 100kg

Maximum load = (558 passengers + 20 crew members) x 100kg = 57800kg

For modification of the value, please refer to the manifest load and FCOM maximum takeoff weight (Flight Crew Operation Manual)

Example (click the double arrows below to expand all codes):


// payload

<[rigidbody][Passengers][]
<[float64][Mass][40000.0]>
<[tmvector3d][InertiaLength][ 30.0 3.0 3.0 ]>
>

View adjustment:

[Overall structure]

The following is the view code structure in this plugin, and some unnecessary codes have been removed.

Example (click the double arrows below to expand the full code):


// cameras

<[camera][CameraLeftWingViewAft][]
<[tmvector3d][R0][ -16.0 3.35 -0.3 ]>
<[tmvector3d][X0][ 0.0 0.0 0.0 ]>
<[tmvector3d][Direction][ 0.36 0.91 -0.1 ]>
<[bool][InCockpit][true]>
<[string8][Tags][cabin window wing flaps left rear]>
>

[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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<[tmvector3d][R0][ α β γ ]>

Example:

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<[tmvector3d][R0][ 31.75 0.52 0.68 ]>

[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.

There must be at least one space before and after α, β, and γ.

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<[tmvector3d][X0][ α β γ ]>

Example:

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<[tmvector3d][X0][ 0.0 0.0 0.0 ]>

[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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<[tmvector3d][Direction][ α β γ ]>

Example:

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<[tmvector3d][Direction][ 0.36 0.91 -0.1 ]>

[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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<[bool][InCockpit][xxx]>

Example:

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<[bool][InCockpit][true]>

Or:

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<[bool][InCockpit][false]>