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IAgAvtrAircraftAcceleration Interface

Description

Interface used to access the acceleration options for an aircraft in the Aviator catalog.

Public Methods

Public Method GetAdvAccelerationByNameGet the advanced acceleration model with the given name.
Public Method GetAsCatalogItemGet the catalog item interface for this object.
Public Method GetBasicAccelerationByNameGet the basic acceleration model with the given name.
Public Method GetBuiltInModelGet the built-in model.

Interfaces

Implemented Interface
IAgAvtrCatalogItem

CoClasses that Implement IAgAvtrAircraftAcceleration

Example

Create a new performance model for an aircraft
[C#]
// Get the acceleration type
IAgAvtrAircraftAcceleration acceleration = aircraft.Acceleration;
// Get it as a catalog item
IAgAvtrCatalogItem accAsCatalogItem = acceleration.GetAsCatalogItem();
// Get the names of the current acceleration models
Array modelNames = accAsCatalogItem.ChildNames;
// Check how many models there are
int modelCount = modelNames.Length;
// Get the child types (for example AGI Basic Acceleration Model, Advanced Acceleration Model)
Array modelTypes = accAsCatalogItem.ChildTypes;
// Create a new performance model of type "Advanced Acceleration Model"
IAgAvtrCatalogItem newPerformanceModel = accAsCatalogItem.AddChildOfType("Advanced Acceleration Model", "Model Name");
// Save the changes to the catalog
aircraft.GetAsCatalogItem().Save();
Configure the basic acceleration performance model of an aircraft
[C#]
// Get the acceleration type
IAgAvtrAircraftAcceleration acceleration = aircraft.Acceleration;
// Get the build in performance model
IAgAvtrAircraftBasicAccelerationModel basicAccModel = acceleration.GetBuiltInModel();

// Get the level turns options
IAgAvtrLevelTurns levelTurns = basicAccModel.LevelTurns;
// Set a max bank angle of 25
levelTurns.SetLevelTurn(AgEAvtrTurnMode.eTurnModeBankAngle, 25);
// Get the climb and descent transition options
IAgAvtrClimbAndDescentTransitions climbAndDescent = basicAccModel.ClimbAndDescentTransitions;
// Set the max pull up G to 1
climbAndDescent.MaxPullUpG = 1.2;
// Get the attitude transition options
IAgAvtrAttitudeTransitions attitudeTransitions = basicAccModel.AttitudeTransitions;
// Set the max roll rate to 25
attitudeTransitions.RollRate = 25;

// Get the aerodynamics
IAgAvtrAircraftAero aero = basicAccModel.Aerodynamics;
// Use simple aerodynamics
aero.AeroStrategy = AgEAvtrAircraftAeroStrategy.eAircraftAeroSimple;
// Get the options for the simple aerodynamics and set some parameters
IAgAvtrAircraftSimpleAero simpleAero = aero.ModeAsSimple;
simpleAero.SRef = 5;
simpleAero.ClMax = 3.1;
simpleAero.Cd = 0.05;

// Get the propulsion
IAgAvtrAircraftProp prop = basicAccModel.Propulsion;
// Use simple propulsion
prop.PropStrategy = AgEAvtrAircraftPropStrategy.eAircraftPropSimple;
// Get the simple propulsion options and set some parameters
IAgAvtrAircraftSimpleProp simpleProp = prop.ModeAsSimple;
simpleProp.MaxThrustAccel = 0.6;
simpleProp.MinThrustDecel = 0.4;
simpleProp.SetDensityScaling(true, 0.02);

// Save the changes to the catalog
aircraft.GetAsCatalogItem().Save();
Create a new performance model for an aircraft
[Visual Basic .NET]
' Get the acceleration type
Dim acceleration As IAgAvtrAircraftAcceleration = aircraft.Acceleration
' Get it as a catalog item
Dim accAsCatalogItem As IAgAvtrCatalogItem = acceleration.GetAsCatalogItem()
' Get the names of the current acceleration models
Dim modelNames As Array = accAsCatalogItem.ChildNames
' Check how many models there are
Dim modelCount As Integer = modelNames.Length
' Get the child types (for example AGI Basic Acceleration Model, Advanced Acceleration Model)
Dim modelTypes As Array = accAsCatalogItem.ChildTypes
' Create a new performance model of type "Advanced Acceleration Model"
Dim newPerformanceModel As IAgAvtrCatalogItem = accAsCatalogItem.AddChildOfType("Advanced Acceleration Model", "Model Name")
' Save the changes to the catalog
aircraft.GetAsCatalogItem().Save()
Configure the basic acceleration performance model of an aircraft
[Visual Basic .NET]
' Get the acceleration type
Dim acceleration As IAgAvtrAircraftAcceleration = aircraft.Acceleration
' Get the build in performance model
Dim basicAccModel As IAgAvtrAircraftBasicAccelerationModel = acceleration.GetBuiltInModel()

' Get the level turns options
Dim levelTurns As IAgAvtrLevelTurns = basicAccModel.LevelTurns
' Set a max bank angle of 25
levelTurns.SetLevelTurn(AgEAvtrTurnMode.eTurnModeBankAngle, 25)
' Get the climb and descent transition options
Dim climbAndDescent As IAgAvtrClimbAndDescentTransitions = basicAccModel.ClimbAndDescentTransitions
' Set the max pull up G to 1
climbAndDescent.MaxPullUpG = 1.2
' Get the attitude transition options
Dim attitudeTransitions As IAgAvtrAttitudeTransitions = basicAccModel.AttitudeTransitions
' Set the max roll rate to 25
attitudeTransitions.RollRate = 25

' Get the aerodynamics
Dim aero As IAgAvtrAircraftAero = basicAccModel.Aerodynamics
' Use simple aerodynamics
aero.AeroStrategy = AgEAvtrAircraftAeroStrategy.eAircraftAeroSimple
' Get the options for the simple aerodynamics and set some parameters
Dim simpleAero As IAgAvtrAircraftSimpleAero = aero.ModeAsSimple
simpleAero.SRef = 5
simpleAero.ClMax = 3.1
simpleAero.Cd = 0.05

' Get the propulsion
Dim prop As IAgAvtrAircraftProp = basicAccModel.Propulsion
' Use simple propulsion
prop.PropStrategy = AgEAvtrAircraftPropStrategy.eAircraftPropSimple
' Get the simple propulsion options and set some parameters
Dim simpleProp As IAgAvtrAircraftSimpleProp = prop.ModeAsSimple
simpleProp.MaxThrustAccel = 0.6
simpleProp.MinThrustDecel = 0.4
simpleProp.SetDensityScaling(True, 0.02)

' Save the changes to the catalog
aircraft.GetAsCatalogItem().Save()
Configure the basic acceleration performance model of an aircraft
[Python - STK API]
      # IAgAvtrAircraft aviatorAircraft: Aviator Aircraft object
# Get the acceleration type
acceleration = aviatorAircraft.Acceleration
# Get the build in performance model
basicAccModel = acceleration.GetBuiltInModel()

# Get the level turns options
levelTurns = basicAccModel.LevelTurns
# Set a max bank angle of 25
levelTurns.SetLevelTurn(AgEAvtrTurnMode.eTurnModeBankAngle, 25)
# Get the climb and descent transition options
climbAndDescent = basicAccModel.ClimbAndDescentTransitions
# Set the max pull up G to 1
climbAndDescent.MaxPullUpG = 1.2
# Get the attitude transition options
attitudeTransitions = basicAccModel.AttitudeTransitions
# Set the max roll rate to 25
attitudeTransitions.RollRate = 25

# Get the aerodynamics
aero = basicAccModel.Aerodynamics
# Use simple aerodynamics
aero.AeroStrategy = AgEAvtrAircraftAeroStrategy.eAircraftAeroSimple
# Get the options for the simple aerodynamics and set some parameters
simpleAero = aero.ModeAsSimple
simpleAero.SRef = 5
simpleAero.ClMax = 3.1
simpleAero.Cd = 0.05

# Get the propulsion
prop = basicAccModel.Propulsion
# Use simple propulsion
prop.PropStrategy = AgEAvtrAircraftPropStrategy.eAircraftPropSimple
# Get the simple propulsion options and set some parameters
simpleProp = prop.ModeAsSimple
simpleProp.MaxThrustAccel = 0.6
simpleProp.MinThrustDecel = 0.4
simpleProp.SetDensityScaling(True, 0.02)

# Save the changes to the catalog
aviatorAircraft.Save()
Create a new performance model for an aircraft
[Python - STK API]
      # IAgAvtrAircraft aviatorAircraft: Aviator Aircraft object
# Get the acceleration type
acceleration = aviatorAircraft.Acceleration
# Get the names of the current acceleration models
modelNames = acceleration.ChildNames
# Check how many models there are
modelCount = len(modelNames)
# Get the child types (for example AGI Basic Acceleration Model, Advanced Acceleration Model)
modelTypes = acceleration.ChildTypes
# Create a new performance model of type "Advanced Acceleration Model"
newPerformanceModel = acceleration.AddChildOfType('Advanced Acceleration Model', 'Model Name')
# Save the changes to the catalog
aviatorAircraft.Save()
Create a new performance model for an aircraft
[MATLAB]
% IAgAvtrAircraft aviatorAircraft: Aviator Aircraft object
% Get the acceleration type
acceleration = aviatorAircraft.Acceleration;
% Get the names of the current acceleration models
modelNames = acceleration.ChildNames;
% Check how many models there are
modelCount = length(modelNames);
% Get the child types (for example AGI Basic Acceleration Model, Advanced Acceleration Model)
modelTypes = acceleration.ChildTypes;
% Create a new performance model of type "Advanced Acceleration Model"
newPerformanceModel = acceleration.AddChildOfType('Advanced Acceleration Model', 'Model Name');
% Save the changes to the catalog
aviatorAircraft.Save();
Configure the basic acceleration performance model of an aircraft
[MATLAB]
% IAgAvtrAircraft aviatorAircraft: Aviator Aircraft object
% Get the acceleration type
acceleration = aviatorAircraft.Acceleration;
% Get the build in performance model
basicAccModel = acceleration.GetBuiltInModel();

% Get the level turns options
levelTurns = basicAccModel.LevelTurns;
% Set a max bank angle of 25
levelTurns.SetLevelTurn('eTurnModeBankAngle', 25);
% Get the climb and descent transition options
climbAndDescent = basicAccModel.ClimbAndDescentTransitions;
% Set the max pull up G to 1
climbAndDescent.MaxPullUpG = 1.2;
% Get the attitude transition options
attitudeTransitions = basicAccModel.AttitudeTransitions;
% Set the max roll rate to 25
attitudeTransitions.RollRate = 25;

% Get the aerodynamics
aero = basicAccModel.Aerodynamics;
% Use simple aerodynamics
aero.AeroStrategy = 'eAircraftAeroSimple';
% Get the options for the simple aerodynamics and set some parameters
simpleAero = aero.ModeAsSimple;
simpleAero.SRef = 5;
simpleAero.ClMax = 3.1;
simpleAero.Cd = 0.05;

% Get the propulsion
prop = basicAccModel.Propulsion;
% Use simple propulsion
prop.PropStrategy = 'eAircraftPropSimple';
% Get the simple propulsion options and set some parameters
simpleProp = prop.ModeAsSimple;
simpleProp.MaxThrustAccel = 0.6;
simpleProp.MinThrustDecel = 0.4;
simpleProp.SetDensityScaling(true, 0.02);

% Save the changes to the catalog
aviatorAircraft.Save();
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