class AirCraft

Inheritance:

Public Methods

AirCraft(Atmosphere* atm)

~AirCraft()

int LoadXML(char* file_name)

Load an aircraft from a XML file.

int ParseXML(xmlDocPtr doc, xmlNodePtr cur)

void OutProperties() const

void OutState()

void Out2File(const double t)

inline void SetRealTime(const double t)

Private Fields

Vector3D Faero

updates all sub-objects moved kinematically

Vector3D Maero

Vector3D Thrust

Aerodynamic forces and moments.

string description

Total Thrust (in Newtons)

double b

AERODYNAMIC RELATED VARIABLES

double S

wing span

double c

wing surface

double xCG

wing chord

double delta_a

control surface deflections

double delta_e

ailerons

double delta_eD

elevator

double delta_r

elevator, differential

double delta_thrust

rudder

double delta_LEF

thrust command

double delta_TEF

leading edge flap deflection

double g

trailing edge flap deflection

double real_time

gravity constant

vector<Engine> engines

to store real time from World and display in HUD

vector<Value> C_values

Aerodynamic variables:

vector<Curve> C_curves

vector<Table> C_tables

Vector2D rudder_lims

limits: +,-

Vector2D aileron_lims

Vector2D elevator_lims

Vector2D LEF_lims

Vector2D TEF_lims

Leading Edge Flap limits

Vector2D stabD_lims

Trailing Edge Flap limits

fstream fileINPUTS

files for output

fstream filelong

fstream filelat

fstream fileFM

Motion SB_mot

forces and moments

Quaternion SB_quat

SpeedBrake motion

double D_SB

Lag stabH_lag

speedbrake drag

Private Methods

void Controls()

Define pure virtual functions of AirDyno

void Kinematics()

Computes all the Control actuations (mapping device inputs to kin/dyn inputs)

void Engines()

Computes all the Kinematics motions before dynamic ones

void Aerodynamics()

Computes the thrust/power of all engines

void GroundReactions()

Computes the aerodynamic forces and moments.

void Dynamics()

Computes the ground forces and moments

void Kinematics3D()

Computes the Rigid Body dynamics.

void UpdateHUD(void)

Set all data needed for HUD

Inherited from AirDyno:

Public Fields

vector<double> continuous_JOY_input

vector<int> button_JOY_input

vector<int> button_KEY_input

Public Methods

inline void SetObject3D(Object3D* obj)

inline void SetObject2D(Object2D* obj)

inline void SetCamera3D(Camera3D* cam)

inline RigidBody* getRigidBody() const

void Simulate(double deltaT)

void Render()

inline void DrawHUD(bool b)

Protected Fields

double dt

RigidBody* rbody

Quaternion Qphys_o3d

AirDataSensor* ADSensor

Atmosphere* atmos

Hud* HUD

bool drawHUD

Camera3D* pilot_camera

Vector3D pilot_eye

Object3D* obj3D

Protected Methods

void UpdateObject3D(void)

void UpdateCamera3D(void)

Documentation

AirCraft(Atmosphere* atm)

~AirCraft()

int LoadXML(char* file_name)

Load an aircraft from a XML file. (0 if OK, 1 if ERROR)

int ParseXML(xmlDocPtr doc, xmlNodePtr cur)

void OutProperties() const

void OutState()

void Out2File(const double t)

inline void SetRealTime(const double t)

void Controls()

Define pure virtual functions of AirDyno

void Kinematics()

Computes all the Control actuations (mapping device inputs to kin/dyn inputs)

void Engines()

Computes all the Kinematics motions before dynamic ones

void Aerodynamics()

Computes the thrust/power of all engines

void GroundReactions()

Computes the aerodynamic forces and moments.

void Dynamics()

Computes the ground forces and moments

void Kinematics3D()

Computes the Rigid Body dynamics.

Vector3D Faero

updates all sub-objects moved kinematically

Vector3D Maero

Vector3D Thrust

Aerodynamic forces and moments. (in body axes)

string description

Total Thrust (in Newtons)

double b

AERODYNAMIC RELATED VARIABLES

double S

wing span

double c

wing surface

double xCG

wing chord

double delta_a

control surface deflections

double delta_e

ailerons

double delta_eD

elevator

double delta_r

elevator, differential

double delta_thrust

rudder

double delta_LEF

thrust command

double delta_TEF

leading edge flap deflection

double g

trailing edge flap deflection

double real_time

gravity constant

vector<Engine> engines

to store real time from World and display in HUD

vector<Value> C_values

Aerodynamic variables:

vector<Curve> C_curves

vector<Table> C_tables

Vector2D rudder_lims

limits: +,-

Vector2D aileron_lims

Vector2D elevator_lims

Vector2D LEF_lims

Vector2D TEF_lims

Leading Edge Flap limits

Vector2D stabD_lims

Trailing Edge Flap limits

void UpdateHUD(void)

Set all data needed for HUD

fstream fileINPUTS

files for output

fstream filelong

fstream filelat

fstream fileFM

Motion SB_mot

forces and moments

Quaternion SB_quat

SpeedBrake motion

double D_SB

Lag stabH_lag

speedbrake drag

This class has no child classes.

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